N91021003
APOLLO
PREPARED
MANUAL
SHEET
DA
TITLE
BY
•
l_aythe on
APPROVAL
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TE
-
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DA TE
BY
TITLE
DA TE
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TITLE
DA TE
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TITLE
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Co.
APPROVED
Raytheon
Co.
APPROVED
MIT/IL APPROVED
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CONFIGURATION
MIT/IL
CONTROL
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TITLE
BY
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RELEASE
BY
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ii
• ND1021003 Apollo Date TDRR
Record
Rev. Let. A
G 21
& N Manual July
1964
11119
of Revisions
Approval Date
3-9-65
TDRR Number I7370
Pages
Revised
i, 111, Iv, v, I-I,
I-3,
I-7,
I-9,
I-II
3-I a 3-2,
4-I,
4-2,
4-3 m 4-5 m 4-9, 4-16 a 4-17 4-21.
4-23.
5"-5m 5-6, 6-5_
A-l
WK
viii
I-5,
2-I t 2-2,
MIT
4-I0,
m 4-18, 4-24_ 5-7,
a A-2
5-8,
NASA WR
4-13,
4-19, 5-2. 6-2,
4-20, 5-4. 6-4,
a B-I
iii
ND1021003 Revision.
AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
LIST THE
OF
TOTAL
EFFECTIVE
PUBLICATION
IS
iii vi
A
ii
Original A
thru
v vii
thru
x
1-2 1-4 1-5 1-6 1-7 1-8 1 -10 1-12
4-1
Original A
thru
4-3
A
thru
4-16
thru
4-21
Original A
4-24
Original A
4 -22 4-23
thru 5-i
Original A
5-2 5-3 5-4
thru
6-3
3-2
Original A
5-7
Original A
6-2
6-4
6-5
Original A
A-2
Original A
thru 7-I
A-l
thru
A
B-I
Original A
4-5 4-6
4-15
Original A
thru
A
thru
6-1
Original A
4-4
THE
Revision
Number
Original A
2-2
2-3 3-I
OF
4-14
Original A
1-11
THIS
4-13
Original A
1-9
thru
Page
Original A
1-3
IN
CONSISTING
Original A
1-1
2-1
,
Original A
viii ix
218
PAGES
:
i
thru
OF
Revision
Number
PAGES
NUMBER
FOLLOWING
Page
A
4-8
Original A
4-9 thru 4-10 4-II thru 4-12
All sheets
Original
JDG's
listed are
part
in of
Appendix this
manual
A
including (
151
data pages)
iv
NO1021003 Revision
A
CONTENTS
Page
Chapter i
DESCRIPTION
LEADING
PARTICULARS
I-I
Introduction
1-1
1-2
Purpose
1-1
1-3
Description
1- 1
i-4
2
AND
of
the
Simulator
1-i
1-1
1-3.1
Logic
1-3.2 1-3.3
D-C Power Supply Assembly Interconnection Plate .
1-3.4
Front
Leading
Plate
Assemblies
Panel
Equipment
I-4.2
Power
1-4. 3
Installation
I-4.4
Cooling
I-4. 5
Operating
Controls
i-4.6
Equipment
History
2- I
Te st Equipment
2-2
Special
1-7 1-7
Supplied
.
Requirements
and
Introduction
3-2
Preparation
1-7
.
1-7
Indicators
1-7 1-7
TOOLS
.
2-1
2-I
.
2-2
USE
FOR
3-I
1-7 1-7
Tools
PREPARATION
.
.
Requirements
SPECIAL
.
.
Requirements
AND
1-5 1-6
.
I-4. 1
EQUIPMENT
.
Assembly
Particulars
TEST
AND
RESHIPMENT.
3-I
3-1 for Use
3-1
Installation
3-1
3-2.2
Interconnection
3-1
3-2.3
Cooling
3-1
3-2.
3-3
AGC
1
Reshipment
.
3-1
ND1021003
CONTENTS
(cont)
Chapter 4
Page THEORY
4-
1
OF
OPERATION
4-I
Introduction
4-2
4-1
General
4-1
Theory
4-2.1
Clock
and
4-2,2
Drive
Rate
4-2,3
Reset
Circuit
4-20
4-2.4
PIPA
Circuit
4-20
4-2.5
PSA
4-2.6
External
4-2.7
Buffer
Circuits
4-2.8
Power
and
SYSTEM
Scaler
4-I
Circuit
.
4-9
Circuit
4-21 Time
Bases
4-22
.
Control
4-23 Circuit
4-24
TIE-IN
5- I
Introduction
5-2
Simulator
CHECKOUT
5-I
5-1 5-1
Interface
AND
ANALYSIS
6-1
6- 1
Introduction
6-1
6- 2
Maintenance
6-1
6-2. i 6-2. 2
6-3
Checkout
6-3.1 6-3.2 6-3.3 6-3.4
6-4
Malfunction
6-1
Periodic Inspection Level of Maintenance
and
6-1 6-1
Calibration
Test Equipment Required Calibration Schedule
6-I
Preliminary Checkout and
6-4
Isolation
Checkout Calibration
and
Analysis
6-4
Procedure
6-4
6-4
vi
ND1021003
CONTENTS
REPAIR
AND
(cont)
7-i
REPLACEMENT.
7- I
Repair
7-i
7-2
Replacement
7-I
7-3
Testing
.
7-I
Appendix A
NUMERICAL THIS
B
LISTING
NUMERICAL WITHIN
OF
JDC's
REFERENCED
MANUAL
A-l LISTING
THIS
WITHIN
MANUAL.
OF
DRAWINGS
REFERENCED B-I
vii
ND1021003 Revision
A
ILLUSTRATIONS
Title
Number
i-i
Apollo
Guidance
Computer
Page
I-2
Logic
Plate
I-3
Logic
Plate,
I-4 1-5
Logic Module
Module and Extraction Tool and Connector Identification
1-6
D-C
I-7
Interconnection
1-8
Front
Assembly Connector
Power
Supply
Panel
AGC
Computer
4-1
AGC
4-2
Clock
4-3
Ring
4-4 4-5
Strobe Strobe
Generator, Waveforms
4-6
Timing
Waveforms
4-7
Drive
Rate
4-8
Burst
Content
4-10
3-Bit
i-6
.
2-3 3-2
Functional
Scaler,
Block
Functional
Logic
+OG
4-12
Programmed
CDU
Block
Diagram
.
Logic Diagram . .
4-4
.
4-5
.
4-6 4-7
Circuit, and
Functional Mode
Block
Circuit,
Functional
.
Burst
Selection
4-I0
Diagram
. Circuit,
Comparator
.
Logic
Diagram
Circuit,
Signal
Circuit,
Logic Logic
Diagram.
4-17
.
4-18
Bias
4-15
Reset
4-16
PIPA
4-17 4-18
PSA Circuit, Logic Power and Control
4-19
Simplified Power and
6-i
Simplified Schematic Diagram AGC Simulator Checkout and Calibration
Circuit, Circuit,
Circuit, Circuit,
Logic Logic
Logic Logic
4-15
Diagram
4-14
Check
4-12
4-14
Selection
J.RIG Bias
4-11
Circuit,
+X
6-3
4-3
Diagram
4-13
Timing Pulse
4-2
Diagram
Diagram
4-II
6-Z
1-8
•
Drawer
Shift Register
Logic
1-5 .
Diagram per
I-4
System
Simulator,
Pulses
I-4
.
Simulator
Counter,
I-3
Layout
Assembly
Calibration
4-9
Module
Assembly
3-1
Block
and
Plate
2-I
and
X
Simulator
1-2
Diagram
4-20
Diagram
Diagram
.
•
4-21
Diagram Diagram Circuit
. for
Schematic Diagram Control Circuit for
Diagram ...... Characteristics
4-21
4-22
. PN
I014061-000, 4-23
PN
1014061-011, 4-24 Flowgram
6-2 6-3 6-5
viii
NO1021003
TABLES
Number
Title
l-I
Equipment
1-11
Operating
Z-I
Test
2-II 5-I
Special Tools AGC Simulator
6-I
Definitions
Supplied Controls
Equipment
and
and
Indicators
Required Required Pin Identification Abbreviations
Page
I-9 I-I0 2-I 2-2 5-2 6-4
ix
ND1021003
Figure
l-1.
Apollo
Guidance
Computer
Simulator
X
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Chapter DESCRIPTION
1-1
LEADING
PARTICULARS
INTRODUCTION
This
technical
calibration, tor, the
AND
I
and
Part
Number
Ground
Company,
Space
The
those
simulator
is
intended
for
systems,
not
intended
use
in
on
1-3
the
in
analyzer.
theory,
(AGC)
I-I)
by
Sudbury
Simula-
is a part
fabricated
Subcontract
is
during
replace
of
Raytheon
Operation,
FNP
of
combination.
to
produce
12775.
drive
optics-inertial the
tests
Analyzer
and
Division,
of ACSP
use
to
(figure
designed
Simulator
for
open-loop
or
System
Simulator
Computer
SIMULATOR
AGC
AGC
of the operation,
Guidance
Systems
part
AGC
the
the
singly
Inertial
as
THE
of of
AGC
(GSE)
Information
OF
purpose
to
tion
The
Equipment and
a description
of the Apollo
Massachusetts,
PURPOSE
tical
contains
1014061.
Support
Sudbury, 1-2
manual
maintenance
AGC
in
various The
these
tests.
guidance
Simulator
(1900005-011).
rate
outputs
subsystem
to
it
navigation
part
ND
The
Rather,
and is
(Refer
iden-
tests.
of
the
1021035
is
subOptics-
for
informa-
)
DESCRIPTION
The
AGC
stallation
Simulator
in
to
facilitate
It
consists
a
access of
supply
panel.
The
inches
wide,
10
imately
lZ
inches
ference
(RFI)
All
are
AGC,
Revision
A
The
without
containing
a hinged high,
high
normal
PSA
although
interior
and
and 19
unit
unit
is
of
the
24
inches
inches
the
logic
unit
plate
panel, deep.
The
provides
from
the
radio
slides rack. a d-c
a hinged
approximately front
in-
rack
assemblies, and
is
for
with
plate,
front
wide,
designed
fabricated
removing three
interconnection
exclusive
inches
self-contained
rack.
front 17
panel,
approx-
frequency
inter-
shielding.
IMU
and
the drawer
assembly,
of the pulse
optics,
to
simulator,
Sixteen
a compact,
19-inch
a logic
power
They
is
standard
and
AGC optics
rates are
inputs CDU
generated available
manually
are
accepted
encoder by with
by
outputs
the AGC essentially
the and
for the the
simulator Av's
from
CDU's, same
buffer the IRIG's,
options
circuits.
PlPA's.
as
PIPA's, in the
controlled.
I-
1
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
.l
,'--4
,.Q
f_ ,_'-4
0
I
, _,..f
.1.-2
HD1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
CONNECTORS
MODULES
" :tlII l
I
ROWS
2
3
4
5
LOGIC
1 6
7
B
9
I0
II
I 12
1314
1516
4
CONNECTORS
PL',TE-MODULE
MODULES
17
]
SIDE
-I
1
i819202122232425262728293031
32333435
/
MODULE
LOCATION
NUMBERS
Y- 7-Y/
PIN
II
IN
PIN
Figure
l-3. 1
LOGIC
contained has
I-3.
PLATE
in three
a maximum
plate
capacity
approximately
designated
A
and
first three
Plate,
Connector
ASSEMBLIES. logic
bly weighs
the
Logic
B.
The
modules
Each
row by
are
occupied
segments
accommodate
the
modules.
modules
are
on
assembly
connection
The sition
made between
plate
logic
and
logic
each
plates
locked
are
for
welded.
inspection
Seven
for the
The Modules
A
typical
modules are
capsulation
keyed of the
are by
or
arranged
is divided a 60-pin
plate
plate
into 35
assemrows,
segments,
connector.
The
between technique.
are
are
logic
in two
Interconnections
different
GSE
simulator.
secured an
The
(HF), gated Connections
logic
module
to the
indexing
made
extraction
are
withdrawn
rethe
Inter-
in the
modules modules
inter-
drawer
are
required
are:
NOR(AC),
logic
a pair
plate
by
under
wrap-around at the end (figure
figure
cap-
the
coupling (CR), resistance-
I-4.
of captive
from
removing with
transformer
screws.
screws.
protection
All
po-
to perform
the captive
farthest I-4).
access
without
to the
flip-flop (KH), interface within the modules are
receptacle
tool
to an
purposes
secured
on
areas
notched
be
is illustrated
two
The
a module
can
troubleshooting plates
provides
accommodate
A
simulator
Each
fitted logic
connectors
and
components
components.
Revision
for the l-Z.)
are
I
IO
Layout
via the wirewrap
output
slide-mounted
(DA), resistor (FD), diode and driver (MK) modules. spot
and
plugs. Logic at each end.
Modules.
functions
plate
assemblies
PIN
by wirewrap.
the interconnection tive screws, one
I-3. t. l
of each
I-3.)
figure
completely
The
maining
connections
segments
figure
A
Module
modules
(See
modules.
15 pounds. (See
logic
assemblies.
of 64
and
20
for the
modules
En-
the
circuit
connector are
labelled
1-3
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Figure
WIRE
I-4.
Logic
Module
and
WRAP
PLATE
WIRE
NO
Extraction
WRAP
PLATE
NO
I 1 ROW
MODULE
LOC
ATIONRO;
MODULE
_j
TYPE PIN
Tool
MODULE
LOCATION
NO
PIN
--
---
NO
NO
Figure
1-5.
Module
and
Connector
Identification
on the logic diagrams with a code to aid in location and identification. ure I-5 is an illustrated description of how to use this code on modules well
as
connector
The NOR
gate.
three A
basic
NPN
gated
these
the stages
within
logic-function NOR
gate
transistors.
flip-flop
Output through
A
pins
module
interface use are
the
simulator.
circuit
element
is an
integrated
The
combination
contains
between
the
eight
to form
contained
circuit of four such
simulator
of transformer-coupled combined
Figas
NOR
and
in the
composed NOR
of a resistor gates
transformer
is a NOR
is a and module.
gates.
the
G
and
common-emitter one
modules
N
is accomplished
stages. driver
Two
of
module.
i-4
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL |1
Two tions
modules
for
module
the
are
logic
containing
Current
limiting
separate
to provide
four
The
"steering"
steering
two-input
diode
is accomplished
with
and
function
gates
and
current-limiting
is provided two
a resistor
single-input
module
func-
with
which
a diode diode
gates.
contains
nine
resistors.
Input
interface
transformer to form
used
circuits.
one
between
the
simulator
coupled
interface
circuit.
interface
coupling
module.
and Four
the
G
and
of these
N
is provided
circuits
are
by
a
combined
_v
Current panel driver
1-3.
is
2
(figure
gain
provided module.
D-C 1-6)
for
the
by
driver
POWER is
mounted
A
in
of
circuits.
SUPPLY
Figure
Revision
illumination
three
Four
ASSEMBLY. the
i-6.
space
D-C
normally
Power
indicator of
these
The
d-c allotted
Supply
lamps circuits
power to
on make
supply logic
plates
the up
front one
assembly 4 and
5
Assembly
1-5
ND1021003 AGCSIMULATOR
in a standard power
ed
GSE
supplies
in inverted by
Two
A
input single
where
the
vdc
which
cable
d-c
is located
I-3.3
INTERCONNECTION in size
undersides
as
a heat
jacks
d-c
and
power
is easily
is If5
supply
supply The
to the
the
of two relays,
and
relays
removed
to power
adjustments
construction
I-7.
supplies
access
assembly the
is composed encapsulated
of the
throughout
PLATE. general
two
sink
for these supply
Figure
assembly and
provide
connects
on the
and
vdc)
cover
is distributed
switch
is similar
The
power
assembly
power
The
+13
in the
Monitor to the
drawer. and
acts
holes
adjustments. The
logic
(+3
positions.
a cover
vicing.
CHECKOUT, MAINTENANCE &REPAIR MANUAL
are
output
single
The
ser-
voltage
on the
cover.
phase,
60
interconnection
assembly
protect-
to facilitate
located
simulator.
cps.
plate,
LOGIC
POWER
also.
interconnection to a logic
Interconnection
are
supply
vac,
modular
all mounted
plate.
plate The
{figure plate
I-7) is
Plate
I-6
ND1021003 AGC SIMULATOR
hinged at the tive screws.
bottom The
ternal
connectors
chassis
hold
1-3.4
FRONT
attached
to screws rear
from
the
rack
the
to
PANEL at
of
1-4
1-4.2
POWER
and
the in
any
60
1-4.5
OPERATING
cfm
to
panel
of
was
cooling
the
air
supply
ulator
that
Revision
at
a
facilitate required
part
of
requires
a
the
AGC
source
of
a current
not
circuits have
part
drain
this
a
of
part of
power
failure
in
PSA
in
0.
event
changed the
1 inch
be
24-inch
depth
part
operating I-6
number
for
NECP
and
the
R-00003
circuit
to
controls 1-8
enable to
a Computer
to
1014061-011.
and
Computer {RIB
of number
approxi-
H20.
figures
Analyzer,
the
was has
designed can
requires
The on
result
Optics-Inertial
number
the
Simulator
shown
ACSP
change
accommodate
AGC
original as
is It
simulator.
are
The
the
Simulator
INDICATORS.
a logic the
the
AGC
pressure
Simulator
However,
from
failure,
static
AND
incorporated
supply does
A
panel
(1900005-011). can
the
The
HISTORY.
1014061.
signal,
power
that
of
CONTROLS
which
power
access
as
of sustaining
The
REQUIREMENTS.
EQUIPMENT
sync
Simulator
capable
rack
height
indicators for the AGC listed in table l-II.
01040031,
AGC
supplied
Analyzer
19-inch
front
mately
ternal
only
provide
indicators
is
by
panel.
equipment
REQUIREMENTS.
standard
COOLING
1-4.6
power
Optics-InertialSystem
1-4.4
Simulator
front
1-8)
and
accessible be withdrawn
front and
the
(figure
to
the
capin-
panel.
corner
are must
of
of
front
assembly
forward
end
side
the
bottom
controls
the
The
single-phase
12-1/4-inch
and are
of
with and
I ampere.
INSTALLATION
mounted
tilted
All
The
REQUIREMENTS.
60-cps,
in
each
each
on
SUPPLIED. table 1-I.
in
of approximately
use
be
each
inside
panel
at
rack.
mounted
on
captive screws the simulator
at
the
are
front
can
Handles
the
at the top the cables
to
PARTICULARS
EQUIPMENT is listed
1-4.3
The
panel
from
simulator
1-4. 1 Simulator
l l5-vac,
with
a pivot
corner. Therefore, front
structure access Stops
The by
plate.
LEADING
for
the
simulator
the
contact
structure
before
the
operate
from
each top the panel.
chassis provide
structure.
ASSEMBLY.
chassis of
the to
chassis
away
interconnection
removal
fastened to tilts forward the
plate
the
the
and plate inside
the
captive from
to
CHECKOUT, MAINTENANCE &REPAIR MANUAL
be
No. an
ex-
supplied Simulator Any
sim-
1014061-000.
1-7
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE 8,REPAIR MANUAL
>,,
r_
o
d !
or-I
1-8
NDi021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Table
1-I.
Equipment
Description Frame Retainer
Part
Number
1014007
support screw
1014013
Frame
1014014-2
Cable
bracket
Channel, Chassis
1014017
bottom
RT
1 0140Z7
bottom structure
LT
1 014028 1 014045-8
Channel,
Cable
assembly
W1
Cable
assembly
W2
Cable
assembly
W3
Support
bracket
Chassis
assembly,
Logic plate Connector
1 014046-i 1 014046-2 1 014046-3 1 014081 dc
1 bracket
power
supply
1 014084 1 014090 1 014094 1014099
Logic
plate
Front
panel
Logic
plate
Cable
assembly
W6
1014112-1
Cable
assembly
W7
1014112-2
Cable
assembly
W8
1014112-3
Cable
assembly
W9
101411Z-4
Inte Cable
Revision
Supplied
A
rconnection assembly
2
1014106 1014110
3
plate
1014113
W4
1014120
i-9
HD1021003 AGC SIMULATOR
CHECKOUT, HAiHTEHAHCE 8,REPAIR HAHUAL
Table
Control
l-II.
Operating
LOGIC
POWER
POWER
POWER
ON
ON
Indicates that +13 the crystal oscillator dicates 115 vac is simulator.
light
switch
Functions
&
Controls
ON
light
SELECT
switch
application
logic
simulator
one
of
OG
C DU,
eight
axes
OPT,
and
voltages
logic
CDU,
for
MG
Y IRIG,
type
BURST, to
Initiates
switch
(IG
the
(SINGLE
START
d-c
voltages
CDU,
Z IRIG,
Y OPT).
EstabIishes
BURST
of
output
X IRIG,
BURST) unit axis. SINGLE
d-c
plates.
Enables
switch
of
to In-
Functions
X Mode
is applied and oven. applied to the
plates.
Indicates
Program
vdc
application
logic
to
DRIVE
Indicators
Functions
to LOGIC
and
or Indicator
Power
STANDBY
Controls
be
one
of pulse CONT,
applied
burst
or
to
of
rate
the
drive
STEADY selected
rate
pulses. switch
PULSES/BURST
Selects
pulse
content
nonadditive 8, per POLARITY
switch
binary
16,
32,
drive
On
d-c
power
supply
any
steps 128,
of
or
256
burst 1,
2,
in 4,
pulses
burst.
Enables tive the
64,
of
either
side DRIVE rate
of
the
the unit SELECT logic
in
positive
or
nega-
axis selected by switch. Inhibits the
OFF
position.
assembly.
1-10
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Table
l-If.
Operating
Controls
and
Indicators
(cont)
I Control
or
Indicator
I Program
IRIG
BIAS
Function
Functions
switch
(cont)
Provides and BIAS
BIAS
REQD
Inhibit
RESET
and
INHIBIT
switch
light
TIMING
INHIBIT
switch
and
light DISABLE switch
DRIVE and
RATE
INHIBIT
bias
RATE
INHIBITED
light
Inhibits
IRIG
dicates
inhibiting
Inhibits
all
hibiting
action.
light
VDC
&
On
Revision
A
d-c
power
reset
function
and
in-
action. and
indicates
in-
generated
signal
and
drive
indicates
action.
presence drive
of rate
externally
inhibit
gen-
signal.
Functions
Provides
light
jack
required
Function
Steady
+3
are
externally
indication
tion.
switch
with
lighted.
outputs
inhibit
erated
SCALER TEST OPERATING and SCALER TEST ON/OFF
IRIG's
Functions
Detects
Test
pulses when
disabling
DRIVE
to
conjunction
light.
IRIG's,
rate
Monitor
in
REQD
Disables
light
pulses
operated
Indicates
light
for
IRIG
biasing
is
Switch to
flash
of
in
ON
at
a
scaler
position 12.
5-cps
on
or
off
indicates
malfunctioning switch is
set
to
or TIMING INIHBIT.
Provides
test
supply
point
for
operacauses rate. scaler
is
INHIBIT
_3
vdc.
assembly.
I- I I
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Table
1-II.
Control
or
Operating
VDC
0 VDC 3 VOLT 13
VOLT
CLOCK
Functions
control
ADJUST SYNC
&
control
(cont)
(cont)
&
ADJUST
Indicators
Function
jack jack
and
Indicator
Test +13
Controls
&
jacks
Provides
test
point
for
+13
Provides
test
point
for
0 vdc.
Controls
output
of
3-vdc
Controls
output
of
13-vdc
points
for
Provides clock
test sync
vdc.
supply. supply. 512-kc
signal.
Fuses 1 AMP
SPARE
blown
FUSE
fuse
indicator
holder On
d-c
power
Provides indication.
ll5-vac
circuit
protection
Provides
storage
for
spare
supply
one
fuse.
assembly.
I-1Z
ND1021003
Chapter
TEST
2- l
TEST
The Simulator
EQUIPMENT
2
AND
SPECIAL
EQUIPMENT
test equipment required is listed in table 2-I.
Table
2-I.
for
maintenance
Test
or
system ure
(see
Model
NASA
calibration
of the
AGC
Required
Part Application
Number
1014217
Clock
oscillator
calibration
fig-
Type
545A
alent;
or
4-channel
trace
preamplifier
Type
M
or
equivalent;
Tektronix,
probes
Precision ferential
DC
(4)
dif-
voltmeter
Type
vdc
po_ver
supply
A
x
10;
Inc.,
Beaverton,
Oregon.
Model alent;
or equivFluke
Model
Wave
analysis
form
Oregon.
P6300
803B John Co.,
Seattle,
analysis
Inc.,
Tektronix,
Mfg.
Waveform
Inc. ,
Oregon.
Beaverton, Scope
equiv-
Tektronix,
13eaverton,
Revision
operation
2- I)
Oscilloscope
+13
or
Equipment
Manufacturers' Equipment
AGC
TOOLS
Waveform
Po_ve r calibration
analysis
supply
Inc.,
Washington 85513
or
alent;
Harrison
Inc., N.J.
Berkley
equiv-
Checkout
Labs, Hgts,
2_ 1
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
TabLe
2-I.
Test
Equipment
Required
Manufacturers' Equipment
Electronic
or
counter
Part
Model
6146
alent,
with
extender,
or
Model
602;
Beckman
Instruments
Bendix
connector
pins,
male
female
crimp
Malco
connector
pins,
Inc.
Frequency and time interval measurements
,
Div., CoL. Corp,
Div., York
Sidney,
Malco
Mfg.
Chicago,
Scintilla New
Co., Ill.
cable
(BNC
- test
Resistors,
prods) 200
ohm
5°'/0 (25)
SPECIAL
TOOLS
The special tools listed in table 2-11.
required
Table
Tool Module tool
Revision
equiv-
(25)
Coaxial
2-2
(25)
female
crimp
+
Bendix
and
Application
Number
Model
Berkley Richmond,
(cont)
A
figure
2-11.
Part
extraction (see
for maintenance
NASA
Special
Tools
of the
Simulator
are
Required
Number 1014018
AGC
Application Logic
module
extraction
1-4)
2- 2
ND1021003 CHECKOUT, MAINTENANCE &REPAIR MANUAL
AGC SIMULATOR
Figure
2-i.
AGC
Calibration
System
Z-3
ND1021003 CHECKOUT, MAINTENANCE &REPAIR MANUAL
AGC SIMULATOR
Chapter PREPARATION
3- 1
FOR
3
USE
AND
RESHIPMENT
INTRODUCTION This
section
tor for
use
contains
by
information
operating
to
necessary
personnel.
Instructions
the
prepare
for
AGC
reshipment
Simula-
are
included
also.
3-2
PREPARATION
FOR
Preparation following 3-2.
for use
entails
1
INSTALLATION.
of the
the performance
of the tasks
described
in the
paragraphs.
the Optics simulator.
Inertial Slides
slides
The
Analyzer. for slide
simulator of space
space.
Slide
of the front the
lowered
The
should
inches
yond
USE
be
travel
panel
original
be
installed
to ND I021035 the simulator
in any
panel
inches.
when
is designed
according
The
plates front
lowered.
approximately
to good
12-I/4
installation
workshop rack
and
inches extend
panel
The
for
practices. requires
7 inches
extends
from
24-1/2
of vertical
panel
above
7-5/8
interconnection
37 degrees
in
for physical location for are supplies. Installation
19-inch
and
Logic
withdrawn.
position
to a position
Refer mounting
the front
is 30
when
Simulator
performed
can
behind
AGC
the
top
inches
plate
can
bebe
the vertical.
WARNING Exercise
care
plates.
Serious
is possible
3-2.2 tem
INTERCONNECTIONS. are
made
Connections The
to display
jacks
are
keyed
in such
mated
jack.
Revision
through
A
located a manner
when
lowering
injury
if plate
All cables
and
test equipment
to fingers
is dropped.
external
two
logic
connected
connections to jacks
are
at the
rear
of the
that
only
the correct
made
simulator. plug
to the
Jl
and
through The can
be
J2
G and (figure
jacks
plugs
and
inserted
J3
N
sys-
3-i). and
jacks
J4. are
into the
3- 1
ND1021003 AGC SIMULATOR
3-2.3
COOLING.
cooling
air
ambient
3-3
CHECKOUT, MAINTENANCE &REPAIR MANUAL
The
at a static
temperature
AGC
pressure
Simulator
requires
of 0. I inch
of 0 to 50 degrees
H20.
approximately
60
cfm
It is designed
to work
of at an
centigrade.
RESHIPMENT
Reship
the AGC
Simulator
Figure
Revision
A
3-i.
in accordance
Computer
with
Simulator
procedure
in JDC
19533.
Drawer
3-2
ND1021003
Chapter THEORY
4-
1
This
chapter
AGC
contains
Simulator.
a discussion
The
plified-logic-diagram generated to
produce
the
the
cuits
required
theory
of
4-2
different
AGC
drive
to
The
prime 4-1,
function is
by
clock
The (3)
reset,
4-2.
1
to
(4)
the
consists
1
2.048-Mc follows Wa,
and
Revision
of
into
is
a
sirn-
waveforms only
the
the
short
for
circuits
simulator
seven
is
basic
discussion
cir-
of
the
The
frequency
which
binary provided
and
of is
wave
fed signals
frequency by
can (1)
The ring
be the
clock the
to
dividing
those
form of
This
and
the
is
Apollo
accom-
modifying
and
the
delayed of
degrees and two
N
4-2)
gen-
system.
to
in
a highly
oscillator
two
divide-by-two
has a
produce
from f2b
of
produces
gates
f2a
circuits.
(figure
up
The
180
buffer
G and
made
and
NOR
these
the
groups for dis(2) drive rate,
It
scaler.
is
week
(7)
circuit
and
circuits. two
and
scaler and
per
of
base,
section
ppl07
through
into seven and scaler,
simulator
division
second
block-diagram
tests.
divided clock
counter,
division the
by
time
lead-in
±4
in
outputs.
external
for
section,
binary
shown identical
subsystem
rate
(6)
pulses
Section.
square
outputs
given
of
and
circuit.
outputs
frequency
SCALER.
timing
108),
the
The
operation
depicting is
divided
Simulator, rate
drive
PSA,
characteristic
pp
of
block-diagram
function
is
optics-inertial
clock
(5)
AND
and
AGC drive
the
a lead-in
aging {_-2
primary
control
in the simulator The groups are:
Lead-In
oscillator term
a
PIPA,
basic of
1.
a
analysis
Included
and
the
the
produce
CLOCK
erates
of
for
logic used purposes.
cussion
the
outputs.
theory
at
illustrations
discussion
power
produce
generating
output
4-2.
to
Computer
plished
on
THEORY
figure
Guidance
the
functional
Detailed Since
the
the
carried
supporting
the
produce of
GENERAL
with
outputs,
operation
is
circuits.
Simulator.
rate
of
discussion
level
in
unique
put
OPERATION
INTRODUCTION
the
on
OF
4
each
stable a
long-
2.048-Mc _2a other.
out
and_2b, Next
divide-by-two stages
two
stages. are
C2,
Wb.
A
4- 1
to
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
I I
CLOCK
WO, I
AND
SCALER
COUNTER RING
I
[
I
I oR,rE RATE C,RCO,T I
i
]ITH. I o'uGH ,'
Wb
LEAD-IN SECTION
, SCALER
I
FOA,
I
SBI
CONTENT
I
I
AND MODE CIRCUIT
l
I
_EL_C, _,oN
I
I
FI3
FOB
I-_
L CLOCK
SBI,
SYNC
SBII, SBO
SBTr +3V
+13V
t EXTERNAL
DR,,,,E RATEI
I
AND
CONTROL CIRCUIT
--
RCU
,
T
I
I
PPB_,
I
B,As
I
CIRCUIT
sB= I ,
TI ME F6,
t
t
POWER
115VAC 60CPS _TIMING INHIBIT_ _REMOTE POWER ON
F4,
C
F7
]
BASE
CIRCUITS
I J CIRCUIT RESET
___
SBI,SBO
CIRCUIT
AND
PIPA
BUFFER
INPUTS
.t. FOR
PN
1014061-011
Figure
Output the
of
512-kc
S3 the
is
module. CLOCK
Revision
one to
coupled CZ is SYNC.
A
the
to
gate
square
input
of
output
act
the
connected
of
F3,
FS,
wave,
is $3
diode
F7
the
NOR
G and
Block
applied
to
on
to
the
permit
gate,
which
a
Diagram
NOR
gate
front
panel.
the
application
controlled Setting of
effectively
by $3
to
IN-
approxi-
inhibits
the
trans
gate
and
circuit.
removes as
Functional
switch
steering
NORMAL to
to
F2,
Simulator,
function a
at
C2
Setting permits C2,
a
AGC
INHIBIT
1 vdc
mission
CIRCUIT
ONLY
forward-biases
mately
PIPA PSA
OPTICS,
AND PIPA OUTPUTS
4-1.
C2,
TIMING
HIBIT
CDU,
CIRCUITS
an
the
inverter N output
also
to
fixed for
circuit J4
and
voltage
C2.
The through
J5
on
the
from output
the of
NOR
the
a transformer front
panel
NOR
gate,
driver and
labelled
4-2
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
2 048MC
2 048MC
512KC
102.4KC
F02 SQUARE
_ICO0_TER i
FO,
l
F05
._
FOA
51,2KC
25.6KC
12,8KC
FI
F2A
F3A
_'T
F28
F3B
6,4KC F4A F4B
DRIVE RATE
32KC
1.6KC
800PPS
FSA
F6A
FTA
FSB
F6B
F7B
400PPS
F8B
200PPS F9A
IOOPPS
5OPPS
25PPS
12, 5PPS
FIOA
FIIA
FI2A
_
FIOB
FIIB
FI2B
_J l
FI3A
÷2 ÷
I_'FI3B 1
OZ_6
Figure
4-Z.
1.2
ZERO
Ring
pulse
signals. vision For will
13
The
at 512
the
and
kc
number
numbers
Scaler,
ring (Wa
Wb)
of flip-flop (five)s
each
The
counter
ring
these
stages
Revision
(SBI,
square of binary
A
generates SBII,
and
waves.
FOA
(figure from
and
and FOB
4-3)
and
of gating
its strobing
five phases SB0)
Block
are
accepts
phases used
nonoverlapping
section
the desired has
both
signal,
of 102.4-kc
two
Diagram
the lead-in
elements
level
if the top gate has Wa as applied, and vice versa.
outputs
Functional
counter
and
example, have Wb
strobe from
odd
Clock
Counter.
trains
Since are
4-2.
(FOA
Wa
gating
frequency and
Wb
the bottom
square and
to trigger
as
waves. NOB)
the
are
diin it.
gate
Three derived
succeeding
division.
4-3
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
t
L
__]
L_
r--'
L
0
©
E
k .,,-i
I
l
l L
1 I
4-'-]
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
F05 F03 FOB
TI
F05 F03
TIMING
INHIBIT
(TI) FOI
J
FOt
Figure
The
strobe
to produce
4-4.
Strobe
generator
signals
SB],
(figure SBII,
and
Generator,
4-4) SB0_
Logic
combines
pairs
Diagram
of ring
counter
outputs
where m
The
four
capability.
Revision
NOR The
A
gates four
SB]
= FOZ
• FO4
• TI
SBII
= FOl
• FO4
• TI
SB0
-- FOl
• FO4
• TI.
with
outputs
inputs of
these
in
parallel gates
provide are
identical
an
increased in
time,
"fan-out' amplitude,
4-5
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE 8,REPAIR MANUAL
FOA
[-i I I I I
SBI
i,I
4LLSEC
7pSEC
H--L
i I I l
,
SBI3
[
_--
+_I 2LISEC
II
b I
I I i
_ _-
5_SEC
t
]
L
i i T_0
Figure
and frequency. of 102.4 kc.
4-2.
1. 3
Scaler.
similar
to
division
is
FOA
The
and
FOB
of
forward
The
and
or
through
widths 10
btsec.
same A
scaler
the
This 12
width
with (10
operating
4-2)
4-3.
first
3 btsec
consists
The
stage
are
is
of
stages
13
are
driven
wide
at
binary two
a
frequency
counter
cascaded,
from
FOA
= FO5
•
FO3
•
TI
FOB
= FO5
•
FO3
•
TI.
and
F1
are
used
to
inhibit
of of
4-5)
so
stages frequency
strobe-like
pulses,
where
be
of
FEA
and
25.
6-kc
process the
are
result
b_sec). indicator
51. as
2-kc
square
timing
10
pulses.
ZERO's
F2B
caused
are
(Refer
all to
circuit
btsec. sneak
by
propagation
used
to
operate
F3A
and
F3B,
inversion
that
for
These
signals, of
waves,
signals
approximately
sneak
coincidence wave.
stage
the
FgB
to
inversions
resultant
of
FZA
untimely square
F1
outputs
principle
of an verse
figure
4-4)
Waveforms
(figure
(figure
The
(figure
These
duration
in
outputs
phase.
F2,
shown
Strobe
pulses
scaler
successive.
Flip-flop of
strobe
The
those
4-5.
and pulses figure is
4-6 built
into
out
causing
the
g uses
pulses
are
stage are is on
timing the
AGC
the
that
same
used
feedresult
of
3 so the
the the
delay
F2A for
degrees
2,
Stage
insertion from
180 stage
in-
the as
that
from
stage
are
basically
down diagram.)
Simulator
so
4-6
of 3
NDi021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
d E E
E
E E
E
E
E 0
F_
q_
b9 v
E:
EZ_
F-
E E
I
J
0
E
E
E
_6
E
I
E q_
c_o
E E
:>p
4-7
HD1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
m o
m m o
m
m u m m
i
m m
rxl m
o
m
m v
0
c_ _.--_
c_ -,--t m .,--I m
I
.S m
I
. ,-.-t
m
i -
1-
LL
_
t_
u_
__
u.
__
g_
if_
4-_
HDi021003 AGC SIMULATOR
that is
the
clozk
done
by
that the 12 cps.
CHECKOUT, MAINTENANCE &REPAIR MANUAL
and
closin_
SCALER If the
circuit INHIBIT.
is
4-2. 2
scaler
not
may
SCALER TEST light is
TEST
"anding"
ing to the
requirements
two
of the DRIVE
signal
PIPA
is 3200
pps
interrogate,
reset
coupled
out.
directly
0) before
being
in one of three configurations (See figure 4-7. )
4-2.
Burst
cuit
1
{figure
or
4-8)
single
ally
Content
with
selecting
switch.
either
of
burst
burst
mode
enables once
so
is
also
1 Burst is a flip-flop
SET
RESET
-- F13A"
START by Logic.
defined
by
+ (8 PPB + (64
PPB
its
SIGNAL"
(SBST + STBSEL) = (I PPB SEL) (F6B) SEL) SEL)
permits
+ (2 PPB
(F9B) (F1ZB)
I"
+ (128
PPB
be
the
for
start
element as
strobed
steady-
up
to
the
80
msec
burst
paise
is
duration
of
con-
received a burst
of
burst
content
ENABLE-
+ (4 PPB
(FIOB) SEL)
the
follows: BURST
(F7B)
SEL)
to of
"not'
logic.
PHA.
SEL)
a
manu-
by
The
content
cir-
logically
rate
logic
principal
+ (16 PPB
drive
mode
continuous,
by
Selection
until
receive and
mode
burst,
controlled
rate
equations
STROBE
and
achieved
switch.
CDU's
accomplished
the
is
drive
The input
is
clock, I, II, or
content
content
axis-selecting
burst
accord-
PIPA
optic
steady is
functio:l
the the
burst
logic.
the
simulator
strobe
the burst
modes
pushbutton
Content
GO
to
the
to
is
(by
and
by
drive
This
controlled
4-2.2.1. logic
rate
inhibits
BURST
IRIG's,
three
This
set
strobed
to the
it is strobed
axis-selecting
msec.
selection
SINGLE
initiated
the
observing
is
is then
equation
operation:
the
switch
continuously
The
Continuous
drive 240
and
of
of
and
approximately and scaler
throughout
signal
controlled
modes.
to
the
every
Single-burst the
the
applied
any
used
The
CDU's,
modes
of
panel
rate of the clock
This
• F5
where
IMU
a
INHIBIT
This
Circuit.
three
Selection panel
continuously
from
Mode
a front
and
maximum tent logic.
and
permits
burst.
The
operation.
front
at off,
outputs.
outputs,
correct
the
rate
= F4D
this rate circuit.
2.
drive
RATE
applied
and
on
TIMING
outputs.
desired
for
flashes steady
the
The
scaler
S13
light on or or
CIRCUIT.
by
quickly
switch
properly
RATE
is formed
This
checked
OPERATING either steady
functioning
DRIVE
be
(FI3B)
SEL)
+ (32
PPB
+ (256
(F8B) SEL) PPB
(FIIB) SEL)
(PHA)
Revision
A
4-9
ND1021003 AGC SIMULATOR
DRIVE
CHECKOUT, MAINTENANCE &REPAIR MANUAL
RATE
PULSES PER BURST SELECT
SINGLE BURST START BUTTON
MONITORING DRIVE RATE
_._
MODE SELECT SWITCH
• LOGIC MODE
}____
I
AXIS SELECTION LOGIC
+ ORSELECT
CDU OUTPUTS IMU
CDU OUTPUTS OPT
DRIVE GATING BIAS
SELECT
OUTPUTS IRIG
_
__[ Figure
This
flip-flop
the pulse SET
4-7.
controls
content
and
RESET
I.
F6B,
of a
256
and
STROBE kpps
5.
BURST drawing
Revision
A
or
burst,
train as
FI0B,
having GO
Diagram
consequently
of bursts.
£1]B,
The
FI2B,
pulse
SIGNAL,
opposite
shift register.
Block
which
REOD TO LIGHTBIAS
]___
terms
establishes used
in the
follows:
10-bLsec
front panel
are
Functional
of the
defined
F9B,
by
PHA
3BI7AC-12. 4.
Circuit,
PPBSEE,
selected
3-bit
SAMPLING
burst are
F8B,
PULSE
LOGIC
duration
frequencies
l through
PHA
Rate
of a given
FTB,
levels 3.
the
equations
scaler 2.
Drive
BIAS
FI3B,
and
FI3A
are
durations.
and
STBSEL
are
d-c
enabling
controls.
polarity (Refer
signals
to drawino_
taken
from
I014063,
the
first
sheet
stage
5, gate
) I is
a
continuous
train
of
3-btsec
pulses
occurring
control
flip-flop.
at
a
10Z.4-
rate. ENABLE 1014063,
is
the
sheet
output 5,
of
flip-flop
a burst
(Refer
to
3AZ2AC-14/16.)
4-I0
HD1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
T_ I PULSE
PER
SINGLE
BURST
BURST
ENABLE
CIRCUIT
CIRCUIT
I
2
BURST
PULSES
PER
STEADY
BURST
BURST _+
ENABLE
BURST
SINGLE
13V
CIRCUIT
CIRCUIT
0 CONTINUOUS
4
PULSES ONE-SHOT
PER
BURST
CIRCUIT
CIRCUIT
B
,, 1
PULSES
PER
BURST
CIRCUIT
16 PER
PULSES
BURST NOR GATE
BURST
GENERATION
CIRCUIT
CIRCUIT
BURST
GATE
T
+(i 32
PULSES
PER
IPH_
BURST
CIRCUIT
-t
I
I 64
PULSES
PER BURST CIRCUIT
12B
I-
3-
BiT
SHIFT REGISTER
PULSES
PER
BURST
CIRCUIT
256
PULSES
PER BURST CIRCUIT
Figure
4-8.
Burst Functional
Content Block
and
Mode
Circuit,
Diagram
4-11
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
F6B I PPB__
____
--
FD
,% ES s, // BURST
d_// /
"t'I3V
SINGLE BURST
(_
SINGLE BURST ENABLE--
CONT
Bo.__
s
FI ! I BURST
END
Figure
4-9.
6.
SBST
7.
GO
is
Figure
Plus $7 for
mately put
of to
of
the
a
vdc
is
1 PPB
NOR
the gate
level.
level
logic
Logic
a one-shot
Diagram
pushbutton
selected
by
of
part
circuit
to
position. resistor
input
of
NOR
as
1 PPB
the
+
switch.
POLARITY
network
diode
acts
a current
NOR
the
following
gate.
gate
are
output
is
of
the
burst
position
was
content chosen
for
follows.
a diode-resistor
the NOR
The
is
is
that
The
The
The
enables
diagram
operation.
the
applied
increased-fan-in
enable
Circuit,
by
enabling
burst of
the
isolation.
the the
Selection
generated
simplified
steady
in
to
Burst
BURST
control.
13
1 volt
or
a d-c
Operation
switch
per
pulse
is
is
during
discussion.
used
single
panel
4-9
used
a
SIGNAL
front
logic
Pulses
GATE
as
limiter The
NOR
PULSES/BURST OR
which
presence gate.
inhibited then
with a passive
a
and
provides of
All as
gate
a ONE;
other
result
NOR of
the
is
approxiat
the
gates
inpri-
absence
F6B.
4-12
NO1021003 AGCSIMULATOR
F6B flop.
appears
PHA,
NOR
at the input
FI3A,
gate
ZERO
CHECKOUT, MAiNTEHAHCE &REPAIR MANUAL
set input.
period
and
ring
12. 5 times
- is selected.
is a series reset
The vides
AND
flip-flop
Since
and
times
the
and
are
causes
the
flip-flop
Another
to
the
NOR
level
the
DRIVE
that a different so that an
B
the
NOR
1,
determined
a by
occurs
o. _ the the
input,
after
the
set.
mode
switch
the appro
B
STEADY
provides
enables
flip-flop
are F6B
to
which
ZERO, the
pro-
flip-flop
set
network
gate
flip-flop
a
NOR to
be
gate
applied
gate.
positions
scaler
enable
of
duration
in the other
flop
setting
a diode-resistor
output
strobing
cept
burst
of $7
frequency gate
is identical
is used
that doubles
to the
for the
one
reset
in duration
discussed
gate
for each
ex-
of the
flip-
advan=e
of
in every
way
is produced.
Single-burst but
one.
shot
No
generator
operation
burst
switch
4-Z.
2.
three
to the
Shift
number
the
Revision
an
A
flip-flop
Register
maintain
output
panel.
of NOR
The
12-volt module,
(figure
burst
gate
switch
2 until a single-
contains
a one-shot
outp,_t that is reduced which,
4-9).
Comparator.
sheet and
of continuous
in turn,
From
to ap-
triggers
this point,
a flip-
operation
is
mode.
and PHB,
PHB to
at the front
approximate
steady-burst
PHA,
simulator. circuit
gate
to that
a resistor
1014063,
outputs:
gister
on the
l volt through
l. 2
drawing
is present
that produces
flop to set the burst identical
gate
is similar
is depressed
proximately
in
to
by
is
(not shown).
of PULSES/BURST
input _sec
SBI
coincidence, This
of
either
ENABLE
of the
output.
reset
when
BURST
position
occur-
- is selected.
in ZERO
A pulses 312
furnished vdc
The burst
RATE
Operation
$7
+13
1.
the the
approximately is
F
of the
at with
reset
applies
allows
present
coincidence to
at the
regardless
80-msec
ZERO
flip-flop
set input
inp,ats are
at the
an
ZERO
_sec.
control
(A) at the
four
is present
p,alses
in
gate
gate
a pulse,
+ nor
10
of the flip-
appear
is a logic
duration
input
is a 10-_sec
neither
every
and
the
second
of
not
This to
NOR
a ZERO
enable
BURST.
occurring
as
FI3A
when
reset
ENABLE
duration
SIGNAL
ONE
enable
When
per
train
pulses
which
ZERO's
GO
at the
BURST
period.
The
of a burst
is set,
four $7.
2,
second.
function.
gate and
the longest ONE
It is a logic
of 3-_sec
NOR
SBI,
has
increased-fan-in
an
mately switch
ONE
_
per
output
to the
SIGNAL,
a 160-msec
+ or
the
GO
and PHC operation
5)
A
triggered
PHC. along
PHA with "n the
3-bit
shift
register
by--and is PHA desired
(refer
F13B
the
only are
one used
of within
to
generates the
three the
used shift
re-
mode.
4-13
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE 8,REPAIR MANUAL
PHA PHB PHC
TO TRIGGER PHC
_
F_3D
4-10.
Since
a
register
must
be
imposed
with
the
the
NOR
gates
ZERO's
ONE
to
100.
at the
The
bination;
as
a
the
of
the
trigger
circuit
thus,
of the
of
F13D
Logic. it to
ting
the
polarity
There
are
switches.
A
lected, ed
the
drive
to
gate be
of
5s
the
shift
to
trigger
cannot
act
Once proper on
the
the of
FOG
the
monitors
the
gate.
is
or
a ZERO.
091
This
resets
rate
DRIVE
axis the
circuit
to
presents
applies
the
a
register
completion
to
of
a
com-
information.
mode This
has been is done
SELECT
When
external
inputs
selected, selec-
by
panel.
CDU.
particular
the
the
partial
front
accomplished
as
010,
which
drive destination.
is
long
100,
permits on
restrictions
This input
than
register, circuit
its
As
NOR
the
is that
coupled
SIGNAL,
axis
Since
example
the other
combinations
typical
PROGRAMMED which
and
sixteen
outp.Jt
rate
the into
2. 2 Axis-Selection necessary to direct
4-10.
increased-fan-in
comparator
axis
to
modes,
modes.
figure
input
Circuit,
different
three
on
combination
4-2. it is
proper
desired
the
of
Comparator
eight
shown
shown,
input
Register Diagram
assume
the
presence
insertion
Shift Logic
can
circuit are
the
3-Bit
provide
comparator
However, all
to
INPUTS
_--
Figure
3-bit
I_
is
both
} and
enabled
electronics. drive
and
rate
OG
and A
POLARITY CDU
allows
are the
seventeenth
continually,
sestrob-
output,
regardless
of
selected.
circuits
for
lection
circuit
is
discussed.
lection
circuit
is
shown
axis
selection A
on
figure
simplified .4-11.
are
similar, logic
Setting
diagram DRIVE
only
the of
the
SELECT
+OG +OG
CDU
se-
CDU
switch
seSll
4-14
NO1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
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4-15
ND1021003 AGCSIMULATOR
to OG
CDU
This
CHECKOUT, MAINTENANCE &REPAIR MANUAL
provides
voltage
a path
is reduced
provides a logic ONE ZERO and is present
for +13
vdc
to forward-bias
to approximately
l vdc
by
input to a NOR gate. The at the input of gate I.
a passive
a resistor
output
diode
module,
of the
NOR
gate. which
gate
is a
",,.._.,-
A
second
gate.
The Gate
by
standard
providing
at the input. is inverted and
INHIBIT
switch
When
of circuit
The
result The
switch
position,
ively
as
input
of gate
and
Sl0
ONE
the
external
shown
2 in conjunction GATE,
used
as
output
by
4-11.
a ZERO.
$4),
with
The
the
It performs
a coincidence a ONE
of
output,
associated DISABLE
vdc
are
DRIVE
applied
SELECT
of the inputs by
loglc. DRIVE
drive
$4
The RATE
inhibit
Sll.
RATE
INHIBIT
OVERRIDE
command
is present
present
inhibit
same
3.
in the
is already rate
switch
DRIVE
4 with
to the
to gate
DISABLE
of gate
a ONE
external
during
3 and Sl0,
external
Since
gate.
provides
+13
at one
input
AND
a NOR
_'q_.
signal.
+ position,
to the
with
and
an
only
gate switch
inhibit
3 is controlled
figure
4 as
from
in conjunction
to gate
on
4 (provided
gates
is present
is applied
of gate
gate BURST
the desired
is set to the
input
A
NOR
l is derived by POLARITY
that is used
other
by
RATE,
This coincidence of ZERO's applied to gate I.
is that a ZERO
$4.
at the
$4,
switch
type
at the
command
input
is effect-
blocked.
A
DRIVE
erator
RATE
With
enable
of drive
then
applied
ing,
isolation,
One programmed
rate and
circuit signal
rate
Revision
levels.
to the
other
continually,
A
driver
occurs The
per
burst
input
present at the
(controlled
by
(figure
4-12). of
input
the
which
gate,
the lamp
of gate I.
Two
in the
form
PULSES/BURST
driver
to the external
in
to gate
a NOR
of gate
commands
discussion
regardless
by
to cause
at the input
to inform
applied
preceded adequate
of a transformer
for circuit
level
required
amplification
is provided
is being
module,
of ZERO's
of ZERO's
lamp
command
to a current
a coincidence
I are
indicator
inhibit
A
command
coincidence
pulses
rate
electronics.
the inhibit
gate
INHIBITED
that a drive
external
drive
of the
function
l is provided
2 is DRIVE
The third input to gate of gate 3 is determined
state
ous
to gate
to gate
2 is one
the AND ZERO's which
input
input
area This axis
the
4 from
amplifies to glow.
3, a simultaneof the
inputs
of "n" switch
module
opthe
at
strobed $7)
for impedance
are match-
electronics.
of
axis-selection
circuit is
is
selected,
used
logic to (This
is
monitor is
the the
true
4- 1 6
HD1021003 AGC SIMULATOR
CHECKOUT, MAINTEHAHCE &REPAIR MAHUAL
+DRIVE
DA
DBS
Figure
only
when
DBS
through
This
permits
2.
4-2.
2. 3
gate
IRIG
for
NOR
Revision
because
of the
an
BIAS
switch
output,
PERMISS
This
SIGNAL
applies (The
of a ONE
an
enable
routing
at the input
GATE+
IRIG
bias
circuit
have
been
driven on.
negative
axes
of the IRIG
STROBE
steady
they
operation
of
gate
2.)
ZERO
(figure on
This and
circuits
level
4-13)
their
is done then
two
II
present
is used
negative by
from
to
axes
simultaneously
on all three
is identical,
or
only
posi-
the
+X
)
this action,
gates.
A
the
SqGNAL
PROGRAMMED RETURN
Diagram
inverter.
The
is initially turned
is discussed.
initiate
The ated
(Since
pushbutton
ZERO
inverter
on all three
PROGRAMMED
REMOTE
3. BURST
when
Logic
to +.
the presence to gate
RATE+
Circuit.
pulses
by
of DBS
Simulator
two
circuit
To
Bias
AGC
tive axes.
BIAS
an
is set
its associated
= DRIVE
the IRIG's
the
IRIG
as
Circuit,
REMOTE
set to OFF.)
switch
2 is inhibited
DBS
3 acts
supplying
is not
1 through
the passage
"normalize" when
switch
to gate
NOTE:
Gate
Signal
that the POLARITY
(a ZERO)
gate
Programmed
the POLARITY
Assume signal
4-12.
I_
on
BIAS
flip-flop the front
4 is set by panel.
This
a one-shot assumes
pulse
from
that gate
the
7 has
a
PERMISS.
circuit
consists
In the continuous
or
of gates steady-burst
5,
6,
and
modes
7 and the GO
their SIGNAL
associand
4- 1 7
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
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ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL tO
the SINGLE
BURST
ZERO,
which
mode,
howevers
ENABLE
always
enables
SINGLE
ZERO.
Therefore,
BURST
is a ZERO.
are
ZERO's;
therefore,
the
set gate
of flip-flop
BURST
the
ENABLE
set gate
the 4.
is a ONE
of flip-flop
output In the
and
the
4 is enabled
of gate
single-burst
GO
only
7 is a
SIGNAL,
when
a
the END
w
Resuming a ZERO, 3.
When
puts),
the discussion
and
a ZERO
F7A
goes
flip-flop
input
of the
is present
gate
rate
pulses
gate
for distribution
for
The
F
10 _sec
flip-flop
This
IRIG
enables
logic
4 is set, set gate
pulse
a ZERO
flip-flop
by STR II to a 3-_sec Simulator.
to the
(normal
is then
4.
resets
to the minus
strobed the AGC
where
at the input
output
for flip-flop
(the first of which
pulses are time within
also
to a ZERO
3 is set.
reset
at the point
width
and the
bias
pulse
for
The
is
scaler
out-
at the
of two
the gate
circuits.
width
output
flip-flop
is present
passage
4) through
F
for
drive
to a NOR drive
to compensate
rate
for
transit
D
Since 4 and any
flip-flop
the
input
further
This
ONE
The
the
resets
gate
of drive
of minus
2 also.
3.
This
This
of flip-flop
axis
command
causes
The matic.
figure
lamp
K2
shown
in turn,
Revision
by
glows
separate
RESET
relay
flop
output
F7A
of flip-flop
from
having
the axis END
causes limits
a ONE
at F.
the minus
axis
two
pulses
command
BURST
on the front
of + AXIS it would pulses
input
pulses by the The
bias
gate
of flip-flop exactly
4
as
COMMAND
are
seem that there is a and the DBS from
generation
at the
panel.
reset
2 to function
circuit
of gate
is inhibited
6.
is neither random nor autooperator when a BIAS REQD check
circuit
is shown
on
to glow.
IRIG
4-14.
Four
by
since
operation
is that
the
I and
generation of the AXIS COMMAND The IRIG BIAS switch is depressed
indicator
BIAS
occurs,
result
thus
from
flip-flops
and applied to gate 9. At first glance A conflict between the AXIS COMMAND
burst
inhibits
3 which
4 and
3 and
8 never
at the F
rate.
generated conflict.
during
The
flip-flop
flip-flops
gate
4.
is present
for flip-flop
F7B
reset
pulses
first pulse
flip-flop
a ONE
the circuit.
of time,
inhibits to two
reset,
set gate
on
a period
command
sets
of the
effect
After
4 is now
in the d-c on
permits
A
signals
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figure the
cause 5-msec
power
4-14. BIAS
the
supply With
REQD
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pulse
REQD
that
section.
lamp
at turn-on.
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pulse
(a ONE)
set,
the F
output
to glow.
The
the flip-flop indicator
indicator
occurs
It is generated sets
the
is a ONE,
indicator
glows
flipwhich, until
4-
19
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
S -Y
IRIG
-Z
IRIG
IRIG
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PULSE
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RESET
R IRIG BIAS HAS
_
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Figure
the
operator
ation
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circuit
The
commands.
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presence
axis
circuit
4-2.
the IRIG
the flip-flop,
at the
IRIG
pulses
3
quency
strobed
with 310
an
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reset
pulse signal
function
this signal
puts:
PIPA PIPA
continuous
Revision
I.
three
NOR
same
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bias
and
axes
produces
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operate
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the
minus
bias
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applied
figure
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of figure
manner
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gate
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is extinguished.
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to initiate
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IMU
of the
4-15.)
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with
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reset
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occurs
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same
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frequency
approximately
be
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307
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I
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after
the preceding
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set
switch.
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The
equation
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IRIG
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one
reset
after
switch
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They
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Logic
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The
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on
as the
identical.
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all derived way
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same
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circuit
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4-16) PIPA
INH
generates CLOCK
two
out-
is a direct
and
follows:
4- 20
HDi021003 AGCSIMULATOR
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CDU
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RETURN DRIVE
RATE
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RESET RESET
RETURN
Figure
4-15.
Reset
Circuit,
Logic
Diagram
DA DRIVEs__o_RATE_
_C_
_-_
PIPA
INT INT
RETURN
DRIVE STROBE RATETF
_
DA
_
PIPA CLOCK P]PA CLOCK RETURN 0244
Figure
4-16.
PIPA PIPA
4-2.5
Revision
PSA
INTERROGATE
CIRCUIT.
A
CLOCK
The
PSA
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Circuit,
Logic
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= F4D
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• STROBE
II
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• STROBE
I.
circuit
(figure
4-17)
A
provides
strobing
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4-21
ND1021003 AGCSIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
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DA
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PSA
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6
EXTERNAL
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Logic
The
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25. 6 kpps
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ND1021003 AGC SIMULATOR
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Figure
4-18.
Power
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Control
Simplified
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Circuit Schematic
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1014061-000,
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4-23
ND1021003 AGC SIMULATOR
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oscillator,
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to
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LOGIC simulator
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panel
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CONTROL
1014061-000,
Simulator
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AND
number
The
for
CHECKOUT, MAINTENANCE &REPAIR MANUAL
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RESET
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Power
and
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Control
Circuit
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Diagram
4-24
HD1021003 AGC SIMULATOR
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TESTING
When
form
performed
located.
accomplished
according
other
it is suggested
in
is
REPLACEMENT
formed
7-3
is
simulator
Replacement
or
REPLACEMENT
REPAIR
AGC site
AND
7
Chapter those
replacements 6 need tests
are not
required
be
made
performed. to
restore
in
the
AGC
Determine the
simulator
Simulator, the
all affected
to
a fully
tests area(s) operable
described and
per-
condition.
7-1
ND1021003
Appendix NUMERICAL
JDC
LISTING
OF
JDC's
A
REI"ERENCED
WITHIN
Number
THIS
Title
04084
AGC
04085
Preliminary
Setup
04086
Preliminary
Turn-on
04087
Frequency
Check
of
Clock
04088
Frequency
Check
of
Continuous
O4O89
Time
Interval
04090
Clock
and
Scaler
Test
1 (Field)
04091
Clock
and
Scaler
Test
2 (Field)
04092
Clock
and
Scaler
Test
3 (Field)
04093
Clock
and
Scaler
Test
4 (Field)
04094
Drive
Rate
Test
1 (Field)
04095
Drive
Rate
Test
2 (Field)
04096
Drive
Rate
Test
3 (Field)
04097
Drive
Rate
Test
4 (Field)
04098
Drive
Rate
Test
5 (Field)
04099
Drive
Rate
Test
6 (Field)
04100
Drive
Rate
Test
04101
PIPA
Clock
04102
External
Time
Base
Test
1 (Field)
04103
External
Time
Base
Test
2 (Field)
04104
External
Time
Base
Test
3 (Field)
04105
Buffer
Tests
04106
Burst
Content
04107
IRIG
04108 04109 04110
Miscellaneous
04131
Malfunction Turn-on
Analysis
for
Preliminary
04132
Malfunction
Analysis
for
Frequency
for
Time
Simulator
Visual (Field)
(Field)
PIPA
Sync
Signal
(Field)
Outputs
(Field)
(Field)
Set
Test
(Field)
(Field) Tests 1 (Field)
IRIG
Test
2 (Field)
IRIG
Test
3 (Field)
Malfunction
(Field)
7 (Field)
and
Continuous
Inspection
Checks
Test
of 04133
MANUAL
(Field)
Simulator
Tests
(Field)
Check
Outputs Analysis
Interval
Checks
Revision
A
A-
1
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE 8,REPAIR MANUAL
Appendix NUMERICAL
JDC
LISTING
OF
JDC's
A
REFERENCED
WITHIN
Number
THIS
MANUAL
(cont)
Title
04134
Malfunction Test 1
Analysis
for
Clock
and
Scaler
04135
Malfunction Test 2
Analysis
for
Clock
and
Scaler
04136
Malfunction Test 3
Analysis
for
Clock
and
Scaler
04137
Malfunction Test 4
Analysis
for
Clock
and
Scaler
04138
Malfunction
Analysis
for
Drive
Rate
Test
1
Drive
Rate
Test
2
04139
Malfunction
Analysis
for
04140
Malfunction
Analysis
for
Drive
Rate
Test
3
Drive
Rate
Test
4
04141
Malfunction
Analysis
for
04142
Malfunction
Analysis
for
Drive
Rate
Test
5
Analysis
for
Drive
Kate
Test
6
Analy
for
Drive
Rate
Test
7
Clock
04143
Malfunction
04144
Malfunction
04145
Malfunction PIPA Set
Analysis Test
for
PIPA
04146
Malfunction Base Test
Analysis 1
for
External
Time
04147
Malfunction Base Test
Analysis 2
for
External
Time
04148
Malfunction Base Test
Analysis 3
for
External
Time
04149
Malfunction
Analysis
for
Buffer
04150
Malfunction
Analysis
for
Burst
04151
Malfunction
Analysis
for IRIG
Test
I
04152
Malfunction
Analysis
for IRIG
Test
2
04153
Malfunction Analysis for IRIG 512-kc Clock Calibration
Test
3
L
04154 _19533
Packaging
04466
Packing
AGC
and
Tests Content
Tests
Simulator
Preliminary Turn-on (Field) AGC Simulator Checkout Information
04234
*From
and
sis
ND
1021035
A-Z Revision
A
ND1021003 AGC SIMULATOR
CHECKOUT, MAINTENANCE &REPAIR MANUAL
Appendix NUMERICAL
LISTING
NASA
Drawing
OF
DRAWINGS
B REFERENCED
Number
1006988
Slide,
1014078
Tool,
1014027
Channel,
Bottom
Right
1014028
Channel,
Bottom
Left
1014045
Chassis
Structure
1014046
Cable
Assembly
1014063
Logic
Flow
1014084
Chassis
1014090
Logic
1014098
Schematic,
Front
I014099
Logic Front
Plate Panel
Assembly
1014106 1014110
Logic
Plate
Assembly
1014112 1014113
Cable Assembly Interconnection
1014117
Schematic,
MANUAL
Chassis Extracting
Diagram
Assembly Plate
DC
Power
Supply
Assembly Panel
Plate
Interconnection
Number
Plate
1014061-000)
I014120
Cable
1014251
Schematic,
Front
1020202
Schematic,
Interconnection
(Part
A
THIS
Title
(Part
Revision
WITHIN
Assembly
Number
Panel Plate
i014061-011)
B- 1
ND1021003
CAUTION: in
The
this
manual
nance,
or
JDC's may
repair
tion
with
SIDL.
and
data
sheet
operation JDC's
and
tained
from
be
and
data
used
for
instructions Only should
the be
on equipment. the associated aperture
sheets
contained
testing,
mainte-
only latest used
after
for
on
file
of
a
performing
Printouts data sheets cards
verifica-
revision of at
JDC any
individual can be oball
sites.
JOB:
VISUAL
INSPECTION
SUBSYSTEM DESCRIPTION: Visual
Rev.
inspection
Date
Let. A 3-9-65
INITIAL
Ground Support AGC Simulator
prior
TDRR
to
Equipment
ASSY'
NO.
l 1 119
D.S. PGS.
and
1014061-011
use.
PAGES
17371
TDRR
JDC: 0408460A06 REV: i014061-000 _A PAGE l_J._OF
--
REVISED
APPROVAL
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT:
INTERVAL: Every
month
TOOLS AND MATERIAL:
PROCEDURE:
1.
Perform
Examine the
interior
condition
freedom 2.
Check
3.
Tighten
and of
such connectors four
the
as
following
exterior
cables,
Allen-head
AGC
logic
good set
and
Simulator,
connectors,
modules, for
of
inspections
switches, plates,
on
VERIFICATION REQUIRED
results.
paying
particular
attention
with
degree
parts
some
to of
etc.
electromechanical screws
and
record
connections. front
panel
for
good
RFI
seal.
Record.
WITH SIDL
BEFORE
USE DATE
21 July
64
1
l._
APOLLO
EQUIPMENT DATA
JDC
G BN TEST
SHEET__L_
JOB:
NO. 04084 REV. A
VISUAL
OF].
AGC
TDRR
11119
INSPECTION
ASSEMBLY TITLE
INITIAL
UNDER
TEST
TEST
Simulator
SER. NO.
DATE DWG.
REV._
MAJOR
H ISTORY
,, START
END
START
END
SITE/LOCATION
TIME
GROUND
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SER.
NO.__ CAL DATE
NAME
SER.
NO.__ CAL DATE
CONDUCTED
BY
APPROVEDBY NAME/AFFILIATION
NAME/AFF
Accept 1.
ILIAT
ION
Reject
Simulator
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
21
July
64
_101_:PRELIMINARY
SETUP
Ground SUBSYSTEM: DESCRIPTION:
AGC
Preparation
Rev. Let. A
Support
_nd
ASSY:
111_? D.S. PGS. REV:A PAGE i0 14061-000 IOF_ i014061-011
I
use.
TDRR
PAGES
NO. 17371
3-9-65
INITIALTDRR JOC: 04085 60A06
--
Simulator
for
Dote
Equipment
REVISED
APPROVAL
JDC
D.S.
MIT
All
All
VV-K
REFERENCES:
NASA WR IMPORTANT:
INTERVAL: Every TOOLS AND _MATERIAL:
30
Two
days
female
connector or
PROCEDURE:
l
o
Perform
Set all able. Use
two
jumper J4U
switches Record. female wires
(high)
and
to
the
the
foliowing
OFF,
crimp-type and J4V
apply
procedure
NORMAL,
connector 115
(common)
vac, on
and
CONT
pins
(Bendix
single-phase rear
VERIFICA REQUIRED
or
external
60
equivalent)
record
the
fully
or cps
CCW
(Bendix
jumpers.
results.
positions
equivalent) to the
connector,
and
crimp-typ_ pins
as
and
Simulator
J4.
applic-
associated via
pins
Record.
TIOH WITH SIDL BEFORE
USE
DATE
21 July
64
_
JDC
APOLLO G 8,N EQUIPMENT TEST DATA
NO. 04085 REV.--_A_
SHEET._!._I OF
JOB:
PRELIMINARY
ASSEMBLY TITLE
AGC
].
INITIAL
1]]19
SETUp
UNDER
TEST
TEST
Simulatqr
SER. NO.
TDRR
HISTORY
DATE DWG.
REV._
MAJOR
GROUND
START
END
SITE/LOCATION
START
END
TIME
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SER.
NO. CAL DATE
NAME
SER.
CONDUCTED
BY
Switches
2.
AC
CAL DATE
APPROVEDBY NAME/AFFILIATION
I.
NO.--
NAME/AFFILIATION
power
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
21
July
64
JOB: PRELIMINARY
TURN-ON (FIELD)
Ground AGC
_UBSY_TEM: DESCRIPTION:
Preliminary
Rev. A
INITIALTDRR JDC: 0408_____6 11119 REV:
--
ASSY:
pane[
TDRR
and
PAGES
NO.
3-9 -65
Equipment
Simulator
front
Date
Let.
Support
power
REVISED
JDC
17371
supply
checks
All
for AGC
APPROVAL
D.S.
All
60A06
D.S. PGS. A__ PAGE_,L_OF
21
1014061-000
Simulator
1014061-i
only.
REFERENCES:
MIT
NASA
ND
1014251
WK
WR
ND
1014117
IMPORTANT:
JDC
04085
must
be
pleted before this procedure formed. Th_s checl_ for PN 000 only. PNl014061-01
Use
JDC i.
04466
com-
is perI014061-
for
INTERVAL: Ever_ TOOLS AND MATERIAL:
30
VTVM
(John
803B (Simpson
PROCEDURE:
i.
2.
Perform
Energize Record. Set
i15
LOGIC
vac
Press
POWER
4.
Set SCALER Record.
5.
Set glow. ND
IRIG
TIMING
ON
TEST
I014117
switch
INHIBIT TEST and
ND
on
POWER
pushbutton.
procedure
and
switch
LOGIC
BIAS
SCALER
following
to simulator
to ON position. Record. 3.
the
check
d-c
ON
BIAS to ON.
switch should
power
supply
should
REQD
LAMP
SCALER
TEST
position.
off or
record
the
that STANDBY
lamp
to INHIBIT go
and
glow
Model
assembly
go
REED
out.
OPERATING
TIMING
steadily.
Read
ON
or
REQUIRED
I-6,ND lamp
I021003)
should
glow.
Record. lamp
INHIBIT no
glows.
should
blink.
lamp
should
continuity
(refer
to
TION WITH SIDL BEFORE
VOM
equivalent)
I014251).
VERIFICA
Model
equivalent);
lamp
(figure
BIAS
should
or 269
Fluke
results.
POWER
glow.
day_s.
USE DATE
21
July
64
_OB:
PRELIMINARY
SUBSYSTEM:
6.
Jlv
Jlw
Jlv
J4n
J 4m
J 4n
J4m
J lw
TIMING
INHIBIT
SCALER
TEST
Read
8.
Using
ASSY:
INHIBIT
switch lamp
to
(refer
NORMAL
should
OPERATING
continuity
go
ND
should
1014117
and
ND
Jlv
Jlw
Jlv
J4n
J4m
J4n
J4m
J lw
VTVM, + 3.0 + 13.0
switch
measure
±
0. 15 vdc ±
0.65
vdc
to and
OF
2
OFF.
Record.
blink.
To
TEST
2,
10]406]-000
60A06
position.
From
SCALER
PAGE
A
out.
lamp
to
REV:
04086
--
To
TIMING
Set
Equipment
From
Return
7.
JDC:
TURN-ON
Ground Support AGC Simulator
I014251):
Record.
record.
at 3-volt
test points
at 13-volt
points
on on
power
power
supply supply
assembly. assembly.
DATE
21
July
64
APOLLO
If
G&N
JDC 04086
INO
EQUIPMENT DATA
TEST
SHEET
JOB:
I__k__OF
1
PRELIMINARY
TURN-ON
ASSEMBLY AGC
TITLE
UNDER
TEST
TEST
HISTORY
Simulator
DWG.
SER. NO.
END
START
END
SITE/LOCATION
[ DATE TIME
REV._
MAJOR
START
GROUND
SUPPORT
TOTAL
EQUIPMENT
NAME
SER. NO.
;NAME
BY
APPROVED
STANDBY LOGIC
POWER POWER
POWER
NAME/AFF
5.
BIAS
REQD
REQD
SCALER TIMING
lamp
ON
BIAS o
on
Lamp
on
TIMING
INHIBIT
INHIBIT
Lamp to INHIBIT
lamp
ILIAT
lamp off or JIv to Jlw J Iv to J4n J4m
to
J4n
J4m
to
J lw
switch
lamp
SCALER
TEST
OPERATING
continuity
TEST
No
blinks
glowing
steady
lamp
blinks
to NORMAL
INHIBIT
SCALER
ION
on
TIMING
No
o
DATE
out OPERATING switch
SCALER TEST No continuity
8.
CAL
on
lamp
lamp
TEST INHIBIT
TIMING
6.
DATE
BY
NAME/AFFILIATION
Yes
4.
CAL
SER. NO._
I CONDUCTED
I. 2.
ELAPSED
out
J lv to J lw Jlv to J4n J4m
to J4n
J4m
to J lw
switch
OFF
Voltages 3 vdc 13 vdc
VERIFICATION REQUIRED
3.0
+
0.15
vdc
13.0
+
0.65
vdc
WITH SIDL
BEFORE
USE DATE
21 July
64
JDC 0__40__87 REV: A JOB: FREQUENCY
Rev.
frequency
Date
of clock
TDRR
Let. A
OF
Ground Support AGC Simulator
SUBSYSTEM DESCRIPTION: The
CHECK
3-9-65
17371
SYN¢
Equipment
sync
PAGES JDC
NO.
CLOCK
signal
--
TDRR
i l 119
D.S. PGS.
1014061-000 60A06
and
I
1014061-001
is checked.
REVISED
APPROVAL
D.S.
All
SIGNAL_INITIAL I | IASSY:
PAGE10F__I
REFERENCES:
MIT
NASA
WK
WR
All
IMPORTANT: must
be
JDC's
04085
completed
and
before
04086
this pro
cedure is performed. INTERVAL: Ever TOOLS AND 'MATERIAL' (Beckman Model
PROCEDURE:
Perform
I.
Allow
45 minutes
2.
Using
coaxial
3.
front
panel
Read
512000.0
Disconnect
the following
of warmup
cable
with
to counter
time
BNC
input.
procedure
for
and
oscillator
connectors, Set
counter
connect to read
record
Z 30
Model 602
or
the
a frequency
6146
with
Extend_
equivalent)
results.
to stabilize. CLOCK
d_£s.
Coaxial cable with BNC connectors, Counter
Record.
SYNC
jacks
of 512
on
kc.
simulator Record.
cps.
counter
from
simulator.
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
21 July
64
r
II
APOLLO GBN EQUIPMENT TEST
JDC
IN0.
04087
lREV.-_A_
DATA SHEET_I JOB:
OF__
FREQUENCY
CHECK
ASSEMBLY AGC
TITLE
IINITIAL
UNDER
OF
CLOCK
SYNC
SER. NO.
SIGNAL
TEST
TEST
Simulator
11119
TDRR
H ISTORY
DATE DWG.
REV._
MAJOR
GROUND
START
END
SITE/LOCATION
START
END
TIME
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SER.
NO. CAL DATE
NAME
SER.
NO._ CAL DATE
APPROVEDBY CONDUCTED
1.
Warmup
g.
Clock
NAME/AFFILIATION
BY
NAME/AFFILIATION
complete sync
51 2000.0
L
VERIFICATION
REQUIRED
cps
WITH 51DL
BEFORE
USE DATE
21
July
64
FREQUENCY JOB:
CHECK
INITIALTDRR
SUBSYSTEM: DESCRIPTION:
A
AGC
Date
Support
of
the
TDRR
continuous
PAGES
NO. 3-9-65
Equipment
17371
outputs
JDC:
are
REVISED
JDC
D.S.
All
All
]!I19
0408__8 REV: _ 1014061-000 ASSY: 60A06
--
S_mulator
frequencies
Rev.
Let.
CONTINUOUS
OUTPUTS Ground
The
OF
D.S. PGS.
I
PAGE 1014061-011 I..]_OF._.L.I and
checked.
APPROVAL MIT
REFERENCES:
NASA
WK
WR IMPORTANT: must
be
cedure
JDC's
04085
completed
and
before
04086 this pro.
is performed.
INTERVAL: Every 60 days. TOOLS AND Counter (Beckman MATERIAL: 6146 with extender 602 with
PROCEDURE:
i.
Adapt pins
Perform
test
the
connectors
specified
in
following
of the
coaxial
following
procedure
cable
as
or equivalent); BNC connectors.
and
record
necessary
to
the
cable
results.
mate
with
rear
connector
steps.
2.
Connect
counter
to
Jld
and
3.
Connect
counter
to
JIL
and
J1K.
Read
and
record
25.6
kpps.
4.
Connect
counter
to
JlZ
and
J1Y.
Read
and
record
25.6
kpps.
5.
Connect
counter
to
J1F
and
J1G.
Read
and
record
12.8
kpps.
6.
Connect
counter
to
Jib
and
Jla.
Read
and
record
3200
pps.
7.
Connect
counter
to
Jli
and
Jlh.
Read
and
record
3200
pps.
8.
Connect
counter
to
J1D
and
JIE.
Read
and
record
800
pps.
9.
Connect
counter
to
J1U
and
JIV.
Read
and
record
800
pps.
10.
Connect
counter
to
J IJ
and
11.
Connect
counter
to
JIM
and
coaxial
mode model
Jlc.
J1H J1N
Read
(PIPA (PIPA
VERIFICA REQUIRED
and
record
clock). set).
Read Read
102.4
and and
kpps.
record record
3200 3200
pps. pps.
TIOH WITH SIDL BEFORE
USE DATE
21 July
64
APOLLO GBN EQUIPMENT TEST
NO.
DATA SHEET
INITIAL
JOB:
]. OF_._L
FREOUENCY
CHECK
OF
CONTINUOUS
AGC
SER. NO.
TEST
Simulator
ASSEMBLY
A
TDRR
llll9
OUTPUTS
TEST TITLE
0c 1
04088
REV..
HISTORY
DATE
UNDER DWG. MAJOR
END
SITE / LOCATION
START
END
TOTAL ELAPSED
TIME
REV._
GROUND
START
SUPPORT
EQUIPMENT
NAME
SER.
NO.
SER.
NO.--
CAL DATE CAL DATE
NAME APPROVEDBY CONDUCTED
BY
NAME/AFFILIATION
NAME/AFFILIATION
2.
I02.4
KPPS
lOZ. 4 kpps
3.
25.6A
KPPS
Z5.6
kpps
4.
25.6B
KPPS
Z5.6
kpps
5.
12.8
6.
]Z00A
PPS
3 ZOO
pps
7.
3Z00B
PPS
3ZOO
pps
8.
800A
PPS
800
pps
9.
800B
PPS
800
pps
10.
PIPA
CLK
3200
pps
11.
PIPA
SET
3 ZOO
pps
KPPS
I 2. 8 kpps
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
2l
July
64
P
JOB:
TIME
SUBSYSTEM: DESCRIPTION: The
Rev.
time
INTERVAL Ground Support AGC Simulator
intervals
Date
JDC
17371
All
JDC: 04089 REV: INITIALGoAo6TDRR 11119
-
IASSY:
signals
PAGES
NO. 3-9-65
Equipment
between
TDRR
Let. A
CHECKS
are
A
1014061-000
and
REVISED
APPROVAL MIT
D,S.
REFERENCES;
NASA
W-K
All
JDCts
04085
must be completed cedure is performed, INTERVAL: Every
60
TOOLS AND MATERIAL: 602
1. 2.
Set
Perform counter
Connect
START
Connect
STOP
Adjust Read 3.
5.
±
STOP
START
Connect
STOP 19.
Connect
Z _sec. counter counter
Z +
Connect
5 +
0.
counter
0.
2 _sec. counter
STOP 117.
2 _sec.
counter
START
Connect Read
counter
0.
START
156.
interval
controls
Connect
Read
time
counter 625
the foIlgwing
counter
Connect
Read 4.
for
counter
Z + 0.
2 _sec.
procedure
and
measurement
input
to
input as
1014081-011
checked.
IMPORTANT:
PROCEDURE:
PAGE__I OF I__ D.S. P_S. I
at
JID
to J1U
and and
or
record
10-nanosecond
and
before
04086
this pro
days. Counter 6146
with
(]Beckman extender
model mod
equivalent)
the
results. resolution.
J1E. J1V.
necessary.
Record. input
to
input
to
Jib Jli
and and
Jla. Jlh.
Record. input
to
input
to
J1L J1Z
and and
JIK. JIY.
Record. input input
to to
Jlb
JIM
and and
Jla. JIN.
Record.
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
21 July
64
APOLLO
GS, N
EQUIPMENT DATA
TEST
SHEET
JOB:
TIME
]. OF INTERVAL
ASSEMBLY TITLE
AGC
lI
1 CHECKS
UNDER
INITIAL
JDC TDRR
11119
(FIELD)
TEST
TEST
Simulator
SER. NO.
NO. 04089 REV. A
HISTORY
DATE
DWG.
REV._
MAJOR
GROUND
START
END
START
END
SITE/LOCATION
TIME
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SERNO.,. CAL DATE"
NAME
SER. NO.__ CAL DATE
i
ICONDUCTED
BY
3.
800A to 800B 3200A to 3200B
4.
25.6A
to 25.6B
5.
3200A
to PIPA
?.,.
APPROVEDBY NAME/AFFILIATION
NAME/AFFILIATION
625
+ 0. 2 _sec
156. 2 + 0. 2 &sec 19.5 ± 0. 2 &sec 117. Z + 0. 2 9sec
SET
VERIFICATION
WITH $1DL
REQUIRED BEFORE USE DATE
21 July 64
JOB:
CLOCK
AND
pulse
characteristics
checked:
Rev. Let A
TEST
Ground Support AGC Simulator
SUBSYSTEM: DESCR IPTION: The
SCALER
25.6A,
CDU
TDRR
Date 3-9-65
INITIAL JDC:
-
timing
characteristics and
REVISED
of the
51Z
11119 REV:
D.$. PGS. _A
i014061-000 following
i
PAGE_I._OF_2 and
I014061-011
signals
are
KC.
APPROVAL
REFERENCES:
JDC
O.S.
MIT
NASA
All
All
WK
WR
17371
TDRR
04090 60A06
ASSY:
I02. 4 KPPS,
PAGES
NO
Equipment
and +OG,
1 (FIELD)
IMPORTANT:JDC,s
04085
must be completed cedure is performed.
and
before
04086 this pro
INTERVAL: Every 60 days. TOOLS AND Os cz_[os cope ('l'ektronix' MATERIAL: 535A, Type M preamplifier, or equiv); Probes (4, Tektronix P6000xl0, or equiv); 8 dum my loads (200 ohm, 4 on female pi 4 on male); jumpers
PROCEDURE:
I.
Perform
Insert
a jumper
from
following
J4A
to
procedure
J4e
and
place
and
loads
25.6A
J1L
and
+OG
J 2C
and
JZB
10g. 4 KPPS
Jld
and
Jlc
51Z
J3T
and
J3S.
KC
2.
Ground
JIK,
3.
Ground
scope
J2B,
Jlc,
on
channel
A
J2C
on
channel
B
Jld
on
channel
C
channel
D.
Sync
scope
5.
Monitor
6.
Monitor (DRIVE
on
and
to Simulator
JIL
J3T ,
the
on
J2Y,
channels channel SELECT
A B
chassis
to ground.
and
D
signal
for for
and
coincident a delay
POLARITY
I
the
results.
from
channel
across:
J1K
J3S.
J2Z
to OG;
record
monitor:
signals.
of 2.0 to +).
+
Record.
0. 2 _sec
A
signal
Record.
VERIFICATION WlTH SIDL REQUIRED BEFORE USE
I
DATE _4
_0B: CLOCK AND SCALER TEST I {FIELD} Ground Support Equipment SUBSYSTEM: AGC Simulator
o
8.
Monitor Check
channel channel
Wave
o
I0.
ll.
D
signal
for the
for
a delay
following
of 2. 0 ±
A
and
from
PAGE
and
channel
2
OF 2
1014061-011
A
signal.
Record
record:
symmetry
Rise
NMT
time
channel
C
for the
following
0. 7 vpp 0. 2 _sec.
characteristics
and
Pulse
amplitude
6 ±
0.6
Pulse
width
3 +
0. 5 Msec
Pulse
rise
Pulse
droop
channels
time
A
and
B
for the
NMT
0. 2 _sec
NMT
0.6
following
v.
characteristics
amplitude
5 ±
0. 5 vpp
Pulse
width
3 +
0. 5 _sec
Pulse
rise
Pulse
droop loads,
time
grounds,
to be performed.
and
jumper.
NMT
0. 2 _sec
NMT
0.6
(Leave
record:
vpp
Pulse
Remove
REV:
i014061-000
0. 2 psec
characteristics
7 +
Check
04090 60A06
ASSY:
Amplitude
Check
are
C
JDC:
and
record:
v. jumper
installed
if further
tests
)
DATE
21
31,1v
64
APOLLO EQUIPMENT DATA
IJ
G 8_N
/NO.
TEST
SHEET_I__
AND
AGC
TITLE
_INITIAL
SCALER
ASSEMBLY
UNDER
TEST
iii19
TDRR
I (FIELD)
TEST
TEST
Simulator
H ISTORY
DATE
DWG.
SER. NO.
o4o9o
IREV.--_
OF_I__
CLOCK
JOB:
JDC
MAJOR
REV.--
START
END
START
END
SITE/LOCATION
TIME
GROUND
SUPPORT
TOTAL
ELAPSED
EQUIPMENT
NAME
SER.
NO. __ CAL DATE
NAME
SER.
NO._ CAL DATE
CONDUCTED
BY
APPROVEDBY NAME/AFFILIATION
NAME/AFFILIATION
5.
Coincidence
6.
Delay
2.0
+
0.
Z _sec
7. 8.
Delay 51Z-kc
2.0
±
0.
Z _sec
+
0.7
Yes
characteristics
Square
wave
symmetry
Yes
Amplitude Rise time 9.
10Z. 4-kpps
No
7.0 NMT
vpp
0. 2 _sec
characteristics
Amplitude Width
6.0
+
0.6
vpp
3.0
+
0.5
Msec
Rise
NMT NMT
time
Droop I0.
No
Channel
A
characteristics
5.0
time
B
characteristics
+
3. 0 + NMT NMT
Droop Channel
_sec v
(25.6A)
Amplitude Width Rise
0.2 0.6
(+OG
0. 5 vpp 0. 5 Msec 0. 2 Msec 0.6 v
CDU)
Amplitude Width
5.0
+
3.0
+
Rise
NMT NMT
time
Droop
VERIFICATION REQUIRED
0.5
vpp
0. 5 #sec 0. 2 Msec 0.6 v
WITH SIDL
BEFORE
USE
DATE
Zl July 64
I
._L.OF..L_ JOB
CLOCK
SUBSYSTEM: DESCRIPTION:
AND
SCALER
Ground Support AGC Simulator
A
TDRR
Date 3-9-65
17371
INITIAL TDRR 11119 IJDC: 0._.4_409.._J.I 60A06 REV: _A
-
ASSY:
and timing 3200A, and
PAGES JDC
NO.
2 (FIELD)
Equipment
The pulse characteristics checked: 25.6A, 25.6B,
Rev. Let.
TEST
relationships 3200B.
REVISED D.S.
All
of the
following
and
signals
1
1614061-0]I
are
REFERENCES:
APPROVAL
All
1014061-000
D.S. PGS. PAGE
MIT
NASA
WK
WR
IMPORTANT: 04090
JDC's
must
this JDC IN TERVAL:
be is
04084,
04085,
completed
an
before
performed.
Every 60 days. TOOLS AND -O-_ET[I-6_cope (_[_-ronlx MATERIAl.,: 545A Type M preamplifi or eQmv_; probes (4, Tektronix P600l)xID, or equiv); 8 d umm_ loa, (200 ohm, 4 on female plns, ton male)
PROCEDURE: 1.
3.
.
Perform
Insert
jumper
from
following
J4A
to J4e
procedure
and
place
and
loads
25.6A
JIL
and
JiE
25.6B
JIZ
and
JiY
3Z00A
Jlb
3Z00B
Jli and
Ground
JIK,
JIY,
Ground
scope
to
Sync
the
and
Jla, Simulator
and
chassis
and
on
channel
A
Jib
on
J1Z
on
channel
B
Jli
on
on
J2Y,
5.
Check
channels
A
6.
Check
channels
7.
Check
channels
JZZ
to
the
results.
across:
Jla Jlh.
J lh.
J1L
scope
record
monitor: channel
C
channel
D.
ground.
B for
180 ° phase
relationship.
B follows
A.
Record.
C and
D
180 ° phase
relationship.
C follows
D.
Record.
C and
D for
one-eighth
rate
and
for
VERIFICATION REQUIRED
coincidence
WITH SIDL
BEFORE
USE
with
channel
A.
Record.
I
I DATE
21 July
64
_10B:CLOCK AND SCALER TEST Z (FIELD) Ground Support AGC Simulator
SUBSYSTEM:
,
Check
the
NOTE:
.
10.
following
Channel
A
ASSY:
characteristics checked
of channels
in JDC
5.0
±
3.0
+
Pulse
rise
NMT
0. Z _sec
Pulse
droop
NMT
0.6
all grounds
channels
A
Remove
through
loads, performed.
and D.
grounds,
scope
A
PAGE
2
OF Z
B,
I0140¢i-000
C,
and
D.
and
I014061-011
Record.
04090.
amplitude width time
REV:
04091 60A06
Pulse Pulse
Reverse
to be
Equipment
JDC:
inputs.
0.5
vpp
0.5_sec
v.
Check
for presence
of inverted
signals,
Record. and
jumper.
(Leave
jumper
installed
if further
tests
are
)
DATE
21
July
64
APOLLO
JDC
G&N
EQUIPMENT
NO. 04091 REV, A
TEST
DATA SHEET 1_!__ OF__ JOB:
CLOCK
AND
SCALER
ASSEMBLY AGC
TITLE
INITIAL TEST
UNDER
Z
(FIELD)
TEST
TEST
Simulator
SER. NO.
iii19
TDRR
HISTORY
DATE
DWG.
REV._
MAJOR
GROUND
START
END
START
END
SITE
/ LOCATION
TIME
SUPPORT
TOTAL
ELAPSED
EQUIPMENT
NAME
SER.
NO.__ CAL DATE
NAME
SER.
NO.__ CAL DATE
BY
CONDUCTED
APPROVEDBY NAME/AFFILIATION
NAME/AFFILIATION
Yes
5.
Channel
B
180 ° from
6.
Channel
D
180 ° from
7.
Coincidence
8.
Channel
B
A C
C
with
A
D
with
A
characteristics
(25.6B)
Amplitude Width
5.0
+
3.0
+
Rise
NMT NMT
time
Droop Channel
C
characteristics
5.0
+
3.0
+
Rise
NMT NMT
time
D
time
Msec
0. 5 vpp 0. 5 _xsec 0. 2 _xsec 0.6 v
inversion,
5.0
+
0.5
vpp
3.0
+
0.5
Ksec
NMT NMT
Droop Signal
0.5
characteristics
Amplitude Width Rise
vpp
0. 2 _xsec 0.6 v
Amplitude Width
Channel
0.5
(3200A)
Droop
9.
No
channels
A
l
through
D
Yes
0. 2 &sec 0.6 v
No
REQUIRED VERIFICATIONBEFORE WITH USE SIDL DATE
21 July
64
JOB:
CLOCK
AND
SCALER
Ground SUBSYSTEM: DESCRIPTION: The
Rev.
Let. A
AGC
pulse
TEST
Support
Equipment
TDRR
JDC: ASSY:
and
PAGES JDC
NO.
3-9-65
INITIALTDRR
-
Simulator
characteristics
Date
3(FIELD)
17371
timing
relationships
REVISED
All
D.S. PGS.
04092 REV: 60A06 I014061-000
of RST
APPROVAL
llll9
IRIG
A
PAGE__!_I OF__.2 and
signals
1
are
1014061-011
checked.
REFERENCES:
O.S,
MIT
NASA
All
WK
WR IMPORTANT: must
be
JDC
's
04085
completed
before
cedure is INTERVAL:
performed.
Every
days.
60
0'4086
and
this
pro-
TOOLS AND-O._lloscope (Tektronix MATERIAL:b4 , Type M preamplifier or equiv);probes (4, Tektronix P6000xl0 or equiv); 8 dum my loads (200 ohm, 4 on female pins, 4 on male); counter (Beckm; model 602 or eouivl
PROCEDURE: 1.
Perform
Insert
jumper
RST
the following
from
J4A
to J4e
IRIG
102.4 Ground
.
J2Z
and
Connect
counter
START
4.
Connect
counter
STOP
5.
Set
counter
4.9
+
.
7.
.
9.
0.2
Disconnect
scope
channel
B.
scope
Measure
and
place
loads
J2Y
and
J2Z
Jld
and
Jlc.
record
the
results.
across:
to J2Y to Jld interval
and and
J2Z.
Jlc.
measurement
(10-nanosecond
resolution)
and
read
Record.
counter.
Ground
Sync
time
_sec.
and
Jlc.
3.
for
procedure
on
to simulator
channel
channel
A
A
chassis
and
monitor
J2Y
on
channel
A
and
Jld
on
signal.
characteristics
as follows
VERIFICATION REQUIRED
and
WITH SIDL
BEFORE
USE
record. J
] DATE
21 July
64
JOB:
CI,C_CK
SUBSYSTEM:
AN/3 SCALER Ground Support AGC Simulator
ASSY:
5.0
±
3.0
±
Pulse
rise
NMT
0. 2 _sec
Pulse
droop
NMT
0.6
all A
II.
Remove
loads, performed,
time
grounds and B.
and scope Record.
grounds,
and
inputs.
jumper.
Check
(Leave
0.5
REV:
1014061-000
amplitude width
Reverse channels
be
JDC:04Q92 60A06
Pulse Pulse
I0.
to
TEST $ (FIELD} Equipment -
PAGE
A and
g
OF 2
1014061-011
vpp
0. 5 _sec v.
for
presence
jumper
of inverted
installed
signals
if further
tests
)ATE
July
on
are
)
21
64
APOLLO
G&N
NO.
EQUIPMENT
TEST
DATA
SHEET_I_
JOB:
CLOCK
OF_L_ AND
AGC
INITIAL
SCALER
ASSEMBLY TITLE
04092
Joc I
REV._
UNDER
TEST
1 1 1 19
3 (FIELD)
TEST
TEST
Simulatoz-
SER. NO.
TDRR
HISTORY
DATE DWG
REV.__
MAJOR
START
END
START
END
SITE/LOCATION
TIME
GROUND
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME NAME
SER.
NO.
SER.
NO.
CAL DATE CAL DATE
APPROVED CONDUCTED
5.
Time
9.
Channel
NAME/AFF ILIATION
interval
4.9
+
0. 2 _sec
Amplitude Width
5.0
+
0.5
vpp
3.0
±
0.5
vsec
Rise
NMT NMT
A
characteristics
(IRIG
RST)
time
Droop i0.
BY
NAME/AFFILIATION
BY
Signal
inversion,
channels
A
and
Yes
B
VERIFICATION REQUIRED
0. 2 Msec 0.6 v
No
WITH SIDL
BEFORE
USE DATE
21
July
64
JDC: JOB:
CLOCK
AND
TEST
Ground Support AGC Simulator
SUBSYSTEM: DESCRIPTION: signal
SCALER
The
are
pulse
Dote
A
3-9-65
{FIELD)
Equipment
INITIALTDRR
A
PAGE_.L_OF_z.
11119
D.S. PGS.
1
60A06
ASSY:
characteristics
REV:
and
timing
1014061-000
relationships
and
of RST
101406_-01]
OPT
checked.
TDRR
Rev. Let.
4
04093
PAGES
REVISED
APPROVAL
REFERENCES:
NO.
JDC
D.S.
MIT
NASA
17371
All
All
WK
WR
IMPORTANT: be is INTERVAL:
JDC's
04085
completed erformed
and
before
this
04086 pro-
60 da,rs. TOOLS AND MATERIAL: lifier,
or
P6000xl0, 200
PROCEDURE:
I.
Perform
Insert
jumper
RST
o
3.
,
5.
Ground
Check
to J4e
and
place
J2X
and
J2W
+OG
J2C
and
JZB.
scope
Observe
J4A
procedure
OPT
JZW
and
on
simulator
with B
switch
following
and
loads
record
the
545A, equiv); or
Type probes
equiv);
4 on
{Tektronix M
preamp(4, Tektronix
8 dummy
female
pins,
loads 4 on
results.
across:
J2B.
J2Y
channel
(POLARITY .
from
Ground scope to on channel B. Sync
the following
ohm,
Oscilloscope
chassis
JZZ
signal to +,
and
monitor
on
channel
A
and
J2C
to ground.
delayed DRIVE
2.0
+
0.2
SELECT
characteristics
switch
of channel 0.5
F_sec from
A
Pulse Pulse
amplitude width
5.0
+
3.0
"+ 0. 5 _sec
Pulse
rise
Pulse
droop
NMT NMT
time
J2X
and
to OG.)
Channel
A
signal.
Record.
record:
vpp
0. 2 _sec 0.6 v.
REQUIRED VERIFICATIONBEFORE WITH USE SIDL DATE
21 July
64
VOB: CLOCK SUBSYSTEM:
.
.
AND SCALER Ground Support AGC Simulator
TEST 4 Equipment
Reverse all grounds and scope on channels A and B. Record. Remove are
to be
loads,
grounds,
performed.
and
(FIELD) -
inputs.
jumper.
JDC: 04093 REV: 60A06 ASSY: 1014061-000
Check
(Leave
for
presence
jumper
A and
0F2
1014061-011
of inverted
installed
2
PAGE
signals
if further
tests
)
DATE
Z1
July
64
APOLLO
EQUIPMENT DATA
, o I Ev.
G BN TEST
SHEET_L_! CLOCK
OF..._L AND
IINITIAL
SCALER
TEST
TDRR
11 119
4 (FIELD)
JOB: ASSEMBLY AGC
TITLE
UNDER
TEST
TEST
Simulator
DATE DWG.
SER. NO.
H ISTORY
REV.--
MAJOR
START
END
START
END
GROUND
SUPPORT
NAME
SER.
APPROVED
BY
NO. -
0. 2 _sec
Amplitude Width
5.0
+
0. 5 vpp
3,0
+
0. 5 Msec
Rise
NMT NMT
delayed from characteristics
A (OPT
time
inversion,
channels
CAL
DATE
RST)
Droop Signal
DATE
BY
+
B A
CAL
NO. --
2.0
Channel Channel
ELAPSED
NAME/AFFILIATION
NAME/AFFILIATION
7.
TOTAL
EQUIPMENT SER.
5. 6.
/ LOCATION
TIME
NAME
CONDUCTED
SITE
A
and
Yes
B
VERIFICATION REQUIRED
0. 2 vsec 0.6 v
No
WITH SIDL
BEFORE
USE
DATE
Zl
July
64
JOB:
DRIVE
RATE
pulse are
1 (FIELD)
Ground Support AGC Simulator
SUBSYSTEM: DESCRIPTION: The CDU
TEST
Equipment
IASSY:
characteristics checked.
Rev. Let.
Date
A
3-9-65
of
TDRR
PDR
PAGES
NO. 17371
JDC: 04094 REV: A INITIALTDRR60A06 11119
-
and
the
timing
JDC
D.S.
MIT
All
All
WK
1014061-000
relationships
APPROVAL
REVISED
PAGE I_L_.OF 2._2__ D.S. PGS. i
between
and
PDR
I014061-011
and
÷OG
REFERENCES:
NASA
IMPORTANT: must
be
JDC's
04085
completed
before
cedure is INTERVAL:
performed.
Every
days.
60
and
04086
this
pro-
TOOLS AND Oscilloscope (Tektronix MATERIAL: 545A, Type M preampli fier or equiv); probes (4, Tektroni P6000xl0 or equiv); 8 dummy loads 200 ohm, 4 on female pins, 4 on rr ale)
)ratory PROCEDURE:
i.
Perform
Insert
a jumper
J4e
J4i
+OG
J2C
and
J2B.
3.
Ground
scope
Check
to
and
J4i
5.
J4A
J4h
Ground
Sync
from
following
PDR
2.
4.
the
and to
Simulator
on
channel
A
J2C
on
channel
B.
on
place
loads
record
the
(Harrison
lab-
results.
across:
chassis
and
monitor:
J4h.
channel
POLARITY
and
and
+13 vdc or equiv)
J2B.
J4h
scope
procedure
supply 855B
B for switch
6.
Set POLARITY Record.
7.
Return POLARITY of channel A and
coincidence to
switch
+.) to
switch record:
with
channel
A.
(DRIVE
SELECT
switch
to
OG,
Record. OFF.
to
I
Note
+ position
absence
and
of
signals
measure
VERIFICATION WITH SIDL REQUIRED BEFORE USE
on
following
I
both
channels
signal
of
scope.
characteristics
DATE 21 July
64
_J08: DRIVE SUBSYSTEM:
D
amplitude
5.0
+
width
3.0
±
Pulse
rise
Pulse
droop
Apply
+13
signal Set
vdc
B
for
signal RATE
DISABLE +13
vdc.
of
on
channel
11.
Reverse on both
12.
Remove are
to
all grounds channels. loads, be
0.6
supply
switch
lamp
RATE
Record.
and Record.
scope
INHIBIT should
inputs.
jumper.
Laboratory
of signal
INHIBIT
DISABLE
and
(Harrison
presence
INHIBITED
lamps
and
2
OF
2-
1014061-011
v
RATE
B.
grounds,
NMT
presence.
Both
1014061-000
PAGE
2 b_sec
INHIBITED DRIVE
external signal
RATE
A
0. 5 bLsec 0.
power
DRIVE
REV:
0. 5 vpp
NMT
Observe
]3.
DRIVE
DRIVE
Return
external J3y.
channel
DISABLE
glow.
from
to pin
on
channel
I0.
ASSY:
Pulse
time
04094 60A06
-
Pulse
equivalent)
o
JDC:
RATE TEST 1 (FIELD) Ground Support Equipment AGC Simulator
on
lamp
channel should
to OVERRIDE DRIVE
should
switch
Check
(Leave
INHIBIT
Monitor
for presence
jumper
glow.
glowing.
to NORMAL
extinguish.
and
position
RATE
remain
855B A
installed
or absence
of
Record. and lamp
monitor should
Record. position.
scope
Remove
for presence
of inverted
if
signals
further
tests
performed.)
DATE
21
July
64
APOLLO
G&N
EQUIPMENT DATA
TEST
SHEET__L__
JOB:
DRIVE
KATE
AGC
TEST
TEST
Simulator DWG.
REV._
START
END
START
END
GROUND
SUPPORT
SERNO.__ SER.
CONDUCTED
BY
Coincidence Absence
7.
Channel
CAL
DATE
NO.__
No
A-B of signals
A
characteristics
(PDR)
Amplitude Width
5.0
+
0. 5 vpp
3.0
+
0. 5 _sec
Rise
NMT NMT
time
Droop Yes
Presence
Lamp Presence
No
of B ON of B
Lamp
ON
Lamp
ON
Presence
of B
Lamps Signal
0. 2 _sec 0.6 v
of A
Absence
I I.
DATE
NAME/AFFILIATION
Yes
6.
CAL
APPROVEDBY NAME/AFFILIATION
i0.
TOTAL ELAPSED
EQUIPMENT
NAME
9.
SITE/LOCATION
TIME
NAME
8.
H ISTORY
DATE
MAJOR
So
11119
1 (FIELD)
UNDER
SER. NO.
JDC TDRR
INITIAL
TEST
ASSEMBLY TITLE
1
OF_A_
NO. 04094 REV. A
OFF
inversion,
channels
A
and
B
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
DATE
z] July
64
JOB:
DRIVE
KATE Ground
SUBSYSTEM: DESCRIPTION: The
pulse
A
2 (FIELD)
Support
Equipment
+IG
CDU,
timing
CDU,
PAGES
and
of the
following
D.S. PGS. 1 A
PAGE_OF and
signals
?-
1014061-0]
are
CDU.
APPROVAL
D.S.
AJI
17371
l l 119
JDC: 04095 60A06 REV: ASSY: 1014061-000
relationships +OG
REVISED
JDC
NO. 3 -9 -65
and
+MG
TDRR
Date
INITIAL TDRR -
Simulator
characteristics
checked:
Rev. Let.
AGC
TEST
REFERENCES:
MIT
NASA
WK
WR IMPORTANT: must
be
JDC's
04085
completed
and
before
04086 this pro
cedure is performed. INTERVAL: Every
60
days.
TOOLS AND Oscilloscope (Tektronix MATERIAL:545A, Type Mpreamplifier or equiv); probes (4, Tektro nix P6000x'10 or equiv); 8 dummy loads (200 ohm, 4 on female pins, 4 on male)
PROCEDURE:
i.
Perform
Insert
a jumper
KST
Z.
place
and
+IG
J ZS and
+MG
J2E JZB,
to Simulator
on
channel
A
J2S
on
channel
B
J2E
on
channel
C
J2C
on
channel
D.
scope DRIVE
on
J4h
SELECT from
and
J2T,
A
with
and
the
results.
across:
JZd J 2B J ZT J2D.
J ZD. chassis
and
monitor:
J4i to ground.
switch by
record
loads and
JZc
delayed
and
J 2C
scope
Set
to J4e
and
J2c
Ground
4.
J4A
procedure
CDU
J2d,
Sync
from
following
+OG
Ground
3.
the
Z. 0 +
to IG 0. Z
and
FLsec.
POLARITY
switch
to + and
observe
channel
B
Record.
VERIFICATION WITH SIDL REQUIRED BEFORE USE
I I
1
DATE
21 July
64
_10B: DRIVE
RATE Ground
SUBSYSTEM.
5.
Set
A.GC
TEST Support
Z
(FIELD) Equipment
JDC:04095 60A06
-
Simulator
DRIVE
ASSY:
SELECT
switch
to MG.
SELECT
switch
to OG.
Observe
REV:
A
PAGE
1014061-000
channel
C
and
delayed
Z
OF
Z
I014061-01
from
A
by
A
by
l
2. 0 +
0. 2 _xsec. 6.
Set
DRIVE
Observe
channel
D
delayed
from
2.0
+
0. 2 _sec. 7.
Measure
the
appropriate and record:
MG,
and
OG,
by
L,n each
means
of the
5.0
+
0.5
vpp
3.0
+ 0.5
Msec
Pulse
rise
Pulse
droop
NMT NMT
Remove are
IG,
characteristics
amplitude width
to be
time
all grounds
all channels B
signal,
signal
Pulse Pulse
Reverse
So
following
with
loads,
and
scope
corresponding
grounds,
performed.
and
inputs. settings jumper.
by
DRIVE
enabling
SELECT
the switch:
0. 2 _sec 0.6 v.
Observe
presence
of DRIVE (Leave
channel
SELECT
jumper
of inverted switch.
installed
signals Record.
if further
)
DATE_
tests
on
[
APOLLO
G BN
EQUIPMENT
TEST
DATA
SHEET__I
JOB:
DRIVE
[REv._A----
OFt_J_ RATE
AGC
[INITIAL
TE.qT
ASSEMBLY TITLE
JDC
]NO. 04095
UNDER
TEST
TEST DATE REV._
DWG.
MAJOR
START
END
START
END
TIME
GROUND
SUPPORT
H ISTORY
SER.
NAME
SER.
APPROVEDBY
BY
NAME/AFFILIATION
B delayed
from
A
Z.O
+
O. 2 _sec
Channel
C
from
A
2.0
+
O. 2 i_sec
A
2.0
+
O. Z _sec
Amplitude Width
5.0
+
0.5
3.0
+
0. 5 Ftsec
Rise
NMT NMT
D A
delayed
delayed from characteristics
(RST
CDU)
time
Droop Channel
B
characteristics
(+IG
vpp
0. Z _sec 0.6v
CDU)
Amplitude Width
5.0
±
0. 5vpp
3.0
+
0. 5 Ftsec
Rise
NMT NMT
time
Droop Channel
C
characteristics
(+MG
Amplitude Width
5.0
Rise
NMT NMT
Channel
+
3. 0 +
time
D
0. 2 _sec 0.6 v
CDU)
Droop characteristics
(+OG
5.0
+
3.0
+
Rise
NMT NMT
time
inversion,
vpp
0. 5 vsec 0. 2 l_sec 0.6 v
Amplitude Width
Signal
0.5
CDU)
Droop ,
NO.
Channel
Channel Channel
7.
NO.
CAL DATE
NAME/AFFILIATION
6.
TOTAL ELAPSED
CAL DATE
CONDUCTED
,
SITE/LOCATION
EQUIPMENT
NAME
5.
11119
Z (FIELD)
Simulator
SER. NO.
TDRR
all channels
REQUIRED
0. 5 Ftsec 0. Z vsec 0.6 v
No
Yes
VERIFICATION
0. 5 vpp
WITH $1DL
BEFORE
USE
DATE
Zl July 64
JOB:
DRIVE
RATE
TEST
Ground SUBSYSTEM: DESCRIPTION:
3 (FIELD)
Support
AGC
Equipment
Simulator
ASSY:
The
pulse
characteristics
and
timing
-IG
CDU,
-MG
-OG
CDU.
Rev.
A
CDU,
and
PAGES
TDRR
Dote
NO.
Let. 3-9-65
INITIAL TDRR JDC: 04096 60A06
-
relationships
REVISED
i014061-000
of the following
APPROVAL
and
J. 2,
i014061-011
signals
are
checked:
REFERENCES:
JDC
D S
MIT
NASA
All
All
WE
WR
17371
11119 D.S. PGS. REV:, A_. PAGE_LOF
MPORTANT: t be
JDC's
04085
completed
cedure
is
and
before
04086
this
pro-
performed.
INTERVAL: Every
60
days.
AND
Oscilloscope
MATERIAL: or
545A
equiv);
probes
P6000xl0 200
Type
or
ohm,
(4,
equiv);
4 on
female
(Tektronix M
preamplifer
Tektronix 8 dummy
loads
_
on
male)
PROCEDURE:
I.
Perform
Insert
a jumper
RST
and and and
-OG
J2N
and
Ground
scope
H,
and
on
channel
J2R
on
channel
B
J2J
on
channel
C
channel
D.
on
scope
on
J4h
POLARITY from
by
place
loads
record
the
results.
across:
J2d J2P J2H J2M.
chassis
and
monitor:
A
with
switch A
and
and
M.
to simulator
J2c
J2N
delayed
J2c
J2J
3.
Set
to J4e
JZR
P,
procedure
J4A
-MG
J2d,
5.
following
-IG
Ground
Sync
from
CDU
2.
4.
the
2.0
J4i to ground. to +
- and 0.2
I
DRIVE _sec.
SELECT
switch
to
IG.
Observe
channel
B
Record.
REOUIRED VERIFICATIONBEFORE WITH USE SIDL
DATEZI
July
64
JOB:
DRIVE
SUBSYSTEM:
6.
7.
8.
9.
Set
10.
DRIVE
SELECT
O. Z _sec.
Record.
Set DRIVE
SELECT
0. Z _sec.
Record.
Measure
signal
IG,
or
MG,
Reverse on
OG,
by
ASSY:
switch
to
switch
to OG.
characteristics means
MG.
on
from
Observe
channel
D
delayed
from
each
channel
0.5
+
0.5
Pulse
rise
Pulse
droop
NMT NMT
loads,
grounds,
to be performed.
scope
and
0.2 0.6
inputs.
enabling switch
Z
OF
1014061-011
A by
A
by
2.0
±
Z. 0 ±
the appropriate
and
2.
signal,
record:
vpp asec i_sec v.
Observe
settings jumper.
by
SELECT +
and
and
delayed
3.0
appropriate
1014061-000
C
5.0
with
PAGE
A
channel
amplitude width
all grounds
REV:
Observe
of the DRIVE
time
04096 60A06
-
Pulse Pulse
all channels
Remove are
JDC:
RATE TEST 3 (FIELD) Ground Support Equipment AGC Simulator
presence
of the DRIVE
(Leave
jumper
of inverted
SELECT installed
signals
switch.
Record.
if further
tests
)
DATE
ZI July
64
,JDC
APOLLO G &N EQUIPMENT TEST DATA JOB:
SHEET__I_ DRIVE
NO.
OF_L
RATE
TEST
ASSEMBLY TITLE
AGC
REV.
A
INITIAL
TDRR
iZlZ?
3 (FIELD)
UNDER
HISTORY
TEST
TEST DATE
Simulator
SER. NO.
04096
REV.__
DWG.
MAJOR
START
END
START
END
SITE
/
LOCATION
TIME
GROUND
SUPPORT
TOTAL
ELAPSED
EQUIPMENT SERNO.
NAME NAME
SER.
CONDUCTED
B
delayed
from
A
2.0
4- 0. 2 _sec
6.
Channel
C
delayed
from
A
2.0
4- 0.2
7.
Channel
D
delayed
from
A
2. 0 4- 0. 2 _sec
8.
Channel
B
characteristics
(-IG
C
Amplitude Width
5.0
+
3.0
4. 0. 5 _sec
Rise
NMT NMT
0. Z F_sec 0.6 v
time
characteristics
(-MG
0. 5 vpp
CDU)
Amplitude
5.0
+
0. 5 vpp
Width
3.0
±
0. 5 _tsec
Rise
time
Droop D
_sec
CDU)
Droop
characteristics
(-OG
NMT
0.2
Dsec
NMT
0.6
_sec
CDU)
Amplitude Width
5.0
+
3.0
4. 0. 5 &sec
Rise
NMT NMT
0. 2 _sec 0.6 v
time
Droop Signal
DATE
NAME/AFFILIATION
ATION
Channel
9.
CAL
NO.--
5.
Channel
DATE
APPROVEDBY
BY NAME/AFFILI
Channel
CAL
inversion,
all channels
REQUIRED
No
Yes
VERIFICATION
0. 5 vpp
WITH $1DL
BEFORE
USE
DATE
Zl
July
64
JOB:
DRIVE
RATE
TEST
Ground SUBSYSTEM: DESCRIPTION: The -X
pulse
AGC
4
Support
+Y
IRIG,
and
TDRR
Rev. Let.
Date
A
3-9-65
Equipment
INITIALTDRR 11119 D.S. PGS. 1 JDC: 0409____._.7REV: A PAGE _J_ OF ..._ 60A06 ASSY: 1014061-000 and 1014061-011
-
Simulator
characteristics
I_RIG,
(FIELD)
and +Z
PAGES
NO. 17371
timing
relationships
of the following
signals
are
checked:
IRIG.
REVISED
APPROVAL
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WIK
WR. IMPORTANT: must
be
cedure
JDC's
04085
completed
and
before
04086
this pro-
is performed.
INTERVAL: Ever
60
TOOLS
AND
da
MATERIAL: fier
or
545A, equiv);
P6000xl0 (200
s.
Oscilloscope
or
ohm,
PROCEDURE:
Perform
Insert
i.
a jumper
RST
3.
.
5.
from
IRIG
J4A
to J4e
and
J2Y
and
J2Z
I_RIG
J2F
and
J2G
+Y
IRIG
JIX
and
JlW
+Z
IRIG
J2k
and
J2j.
J2Z,
Ground
scope
G,
j, and
on
channel
A
JZF
on
channel
B
JIX
on
channel
C
J2k
on
channel
D.
scope
on
delayed
loads
record
the
preampliTektronix
8 dummy
female
loads
pins,
(Beckman602 Model
4 on
model or equiv)6146
results.
across:
chassis
and
monitor:
J2Y. switch
from
place
and
equiv),
M (4,
JlW.
to Simulator
J2Y
Set POLARITY B
procedure
+X
Ground
Sync
the following
Type probes
4 on
wmale); counter .... ith Extender
(Tektronix
A
to + and
approximately
DRIVE
SELECT
5 btsec.
VERIFICATION REQUIRED
switch
to X
IRIG.
Observe
channel
Record. WITH SlOg
BEFORE
USE
[
I
DATE .._
4
JOB:
DRIVE
RATE
SUBSYSTEM:
6.
Set
Set
DRIVE
Set IRIG on channel
9.
Return
II.
switch
switch
5 btsec.
Record.
RESET A.
INHIBIT Record.
Measure
RESET
the to
Observe
channel
to
Z
Observe
channelD
following
IRIG.
switch
INHIBIT.
switch
signal
signals
to
to
Monitor
characteristics,
on
channels
using B,
C,
and
amplitude
5.0
+
0.
width
3.0
+
0. 5 _tsec
Pulse
rise
Pulse
droop
time
all ground as
grounds
and
selected
12.
Return
13.
Connect
START
counter
14.
Connect
counter
STOP
C
iO]4nA]-nt]
and
delayed
from
A
approx-
delayed
from
A approx-
by
to original
of 4.9
+
NMT
0. 2 btsec
NMT
0.6
scope
inputs.
DRIVE
Observe
SELECT
to J2Y
to JZF
and
0. 2 btsec.
J2G
(DRIVE
and and
and
JlX.
Record.
16.
Repeat
step
14 for +Z
IRIG
and
J2k.
Record.
17.
Remove
performed.
remove
measure
SELECT
IRIG
jumper.
absence
of
signal
SELECT
switch
as
nec-
record:
of inverted
signals
on
Record. scope
probes.
J2Z.
14 for +Y
and
and
presence
and
step
grounds,
DRIVE
D
switch.
Repeat
loads,
for
v .
configuration
input
scope
5 vpp
15.
to be
OF 2
2
NORMAL.
Pulse
resolution)
1014061-000
Y IRIG.
Pulse
all channels
PAGE
A
60A06
to
INHIBIT
enable
Reverse
REV:
04097
-
Record.
SELECT
IRIG
essary
-
ASSY:
SELECT 5 _sec.
8.
JDC:
Equipment
Simula_oI"
DRIVE
imately
10.
Support
A_
imately 7.
4 (FI£LD)
TEST
Ground
(Leave
time switch
jumper
interval in X
installed
(10-nanosecond
IRIG
if
position.
further
) Record.
tests
are
)
DATE
21
July
64
APOLLO
EQUIPMENT DATA
JDC
G&N TEST
SHEET_
JOB:
NO. 04O97 REV. A
DRIVE
RATE
TEST
ASSEMBLY TITLE
INITIAL
OF_L_
AGC
TDRR
llll9
zl (FIELD)
UNDER
TEST
TEST
H ISTORY
DATE
Simulator
SER. NO.
DWG.
END
START
END
SITE/LOCATION
TIME
REV,_
MAJOR
START
GROUND
SUPPORT
TOTAL
ELAPSED
EQUIPMENT SER.
NAME
SER.
NAME
NO.. CAL
DATE
CAL
DATE
0.5
vpp
NO.
APPROVEDBY NAME/AFFILI
NAME/AFFILIATION
ATION
Yes
5.
Channel
B
delayed
from
A
approx
5 bsec
6.
Channel
C
delayed
from
A
approx
5 Ftsec
7. 8.
Channel Absence
D
delayed
from
A
approx
5 bsec
I0.
Channel
B
characteristics
(+X
No
IRIG)
Amplitude Width
5.0
Rise
NMT NMT
time
Droop Channel
C
characteristics
(+Y
5.0
Rise
NMT NMT
0. 2 bsec 0.6 v
+
3. 0 +
time
Droop D
characteristics
(+Z
0. 5 _sec
IRIG)
Amplitude Width
Channel
+
3. 0 +
0.5
vpp
0.
5 btsec
0. 2 0.6v
btsec
IRIG)
Amplitude Width
5.0
±
3.0
+
Rise
NMT NMT
time
Droop Yes
0. 5 vpp 0. 5 gsec 0.2 0.6
F_sec v
No
II. 14.
Signal inversion, Time interval A
all channels to B
4.9
±
0.2
_sec
l 5.
Time
interval
A
to C
4.9
±
0.2
_sec
16.
Time
interval
A
to D
4.9
±
0.2
>sec
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
DATE
zz July 64
JOB:
DRIVE
RATE
TEST
Ground SUBSYSTEM: DESCRIPTION: The
pulse
-X
AGC
-Y
A
3-9
and
-Z
timing
17 371
relationships
of
the
111 lq REV:_._._A
1014061-000
and
signals
following
REVISED
APPROVAL
D.S.
MIT
NASA
All
All
WK
WR
are
JDC's
Every TOOLS
MATERIAL:
with
insert
a jumper
RST
.
3.
,
5.
J4A
to J4e
JZY
and
and
IRIG
J2K
IRIG
J2n
and
Jgm
-Z
IRIG
J2p
and
J2q.
Ground
scope
m,
and
on
channel
A
J2K
on
channel
B
J2n
on
channel
C
J2p
on
channel
D.
scope POLARITY
channel
B
on
place
loads
this
record
the
Type
equiv),
4 on
extender
(Tektronix M
probes
counter
pro
8 dummy
female
pins,
(Beckman model
preampli-
(4, Tektroni
602
loads 4 on
model or
6146
equiv)
results.
across:
J2L
q.
to Simulator
J2Y
and
before
04086
JEZ
-Y
L,
and
procedure
-X
J2Z,
Set
from
IRIG
Ground
Sync
the following
or
ohm,
male);
545A,
equiv);
P6000x10 (200
and
60 days. AND Oscilloscope
fier or
I.
checked:
04085
must be completed cedure is performed. INTERVAL:
Perform
1014061-011
REFERENCES:
JDC
IMPORTANT:
PROCEDURE:
D.S. PGS. 1 PAGE .._._OF..._.
IRIG.
PAGES
NO.
-65
INITIAL TDRR JDC: .04098 60A06
-
ASSY: and
TDRR
Dote
Equipment
Simulator
IRIG,
Let.
(F_ELD)
Support
characteristics
IRIG,
Rev.
5
chassis
and
monitor:
JZY. switch
delayed
from
to - and A
DRIVE
SELECT
approximately
5 b_sec.
VERIFICATION REOUIRED
switch
WITH SIDL
BEFORE
USE
to X
IRIG.
Observe
Record. I
I
DATE
21
July
64
_0B:DRIVE RATE TEST 5 (FIELD) Ground Support Equipment -
JDC:
SUBSYSTEM:
ASSY:
AC, C
Sim,,l_Qr
6.
Repeat
step
5 for
Y
IRIG
and
channel
C.
Record.
7.
Repeat
step
5 for
Z
IRIG
and
channel
D.
Record.
8.
Measure
the following
necessary
9.
to enable
signal signals
characteristics, on
B,
C,
Pulse
amplitude
5.0
+
0. 5 vpp
Pulse
width
3.0
+
0. 5 _sec
Pulse
rise
Pulse
droop
Reverse
time
all grounds
all channels
as
grounds
and
selected
I0.
Return
I I.
Connect
counter
START
12.
Connect
counter
STOP
resolution)
scope by
to original
of 4.9
+
input
JZn
and
J2m
14.
Repeat
step
12 for
JZp
and
J2q
15.
Remove
and
and
JZL
(DRIVE and and
jumper.
Y Z
DRIVE
and
and
D
remove
A
-000
PAGE and
SELECT
Z
OF
1014061
2
-(]I 1
switch
as
record:
presence
switch. and
REV:
60A06 1014061
using
Observe
SELECT
and
_sec.
12 for
grounds,
v.
to JZY
step
loads,
_sec
0.6
configuration
Repeat
performed.
0.2
NMT
DRIVE
to J2K 0.2
NMT
inputs.
13.
to be
channel
04098
of inverted
signals
on
Record. scope
probes.
J2Z.
and
measure
SELECT IRIG. IRIG. (Leave
time switch
interval to X
(10-nanosecond
IRIG
position.
) Record.
Record. Record. jumper
installed
if further
tests
)
OAT E .?_hj_i_
are
APOLLO
JDC
G&N
EQUIPMENT
NO. 04098 REV. A
TEST
DATA
SHEET.
JOB:
DRIVE
J__ OF__L RATE
TEST
ASSEMBLY TITLE
AGC
INITIAL 5 (FIELD)
UNDER
TEST
TEST
DWG.
START
END
START
END
GROUND
SUPPORT
SER. SER.
NAME
BY
5.
Channel
B
delayed
from
A
approx
5 btsec
6.
Channel
C
delayed
from
A
approx
5 btsec
7.
Channel
D
delayed
from
A
approx
5 b_sec
8.
Channel
B
characteristics
(-X
NO.-CAL
DATE
CAL
DATE
NO..
No
Amplitude Width
5.0
+
3.0
4- 0.
Rise
NMT NMT
time
C
characteristics
(-Y
Amplitude Width
5.0
Rise
NMT NMT
Channel
characteristics
(-Z
5.0
Rise
NMT NMT
Droop
Channel Channel Channel
B C D
delayed delayed delayed
Yes
all channels from from from
0.5
vpp
0. 5 btsec 0. 2 Msec 0.6 v
+
3. 0 ±
time
inversion,
±
IRIG)
Amplitude W id th
Signal
vpp 5 bzsec
0. 2 i.tsec 0.6 v
3. 0 ±
time
D
0.5
IRIG)
Droop
14.
ELAPSED
IRIG)
Droop
13.
TOTAL
NAME/AFFILIATION
Yes
Channel
ION
APPROVEDBY NAME/AFFILIATION
12.
/ LOCAT
EQUIPMENT
NAME
CONDUCTED
SITE
TIME
REV.__
MAJOR
9.
H ISTORY
DATE
Simulator
SER. NO.
11119
TDRR
0.5
vpp
0. 5 btsec 0. 2 b_sec 0. 6 v
No
A
4.9
+
A
4.9
+
0. 2 btsec
A
4. 9 ±
0. 2 bLsec
VERIFICATION REQUIRED
0. 2 _sec
WITH SIDL
BEFORE
USE
DATE
Zl /uly 64
00B:DRIVE
RATE
TEST
Ground $UBSYST£M: DESCRIPTION: The pulse +X OPT
Rev.
A
Equipment
INITIALTDRR 11119 D S. PGS. 1 JDC: 04099 REV: A.____ PAGE_I__OF_2._. 60A06 ASSY: 1014061-000 and 1014061-011
-
Simulator
characteristics and +Y OPT.
and
timing
PAGES
TDRR NO.
_-9-65
(FIELD)
Support
AGC
Date
Let
6
17371
relationships
REVISED
JDC
O.S.
All
All
of
APPROVAL MIT
the
following
signals
REFERENCES:
W-R
must
be
Every TOOLS
I.
Insert
a jumper RST
OPT
and
J2W
and
JIB
+Y
OPT
Jlp
and
Jlq.
Ground
scope
B 6.
and
JIG
3.
Set
J4e
J2X
J2W,
5.
to
OPT
Ground
Sync
J4A
procedure
+X
2.
4.
from
following
JIB,
and
on
channel
A
JIC
on
channel
B
Jlp
on
channel
C.
scope
on
POLARITY delayed
Repeat
from
step
place
loads
before
or
545A,
equiv);
record
04086
this
pro..
(Tektronix" Type
probes
or equiv); 4 on female
the
M (4,
preampliTektroni:
8 dummy _ins.
4
load., nn
results.
across:
Jlq.
to simulator
J2X
and
and
60 days. AND Oscilloscope
P6000xl0 200 ohm.
the
04085
performed.
MATERIAL: fier
JDC's
completed
cedure is INTERVAL:
Perform
checked:
NASA
IMPORTANT:
PROCEDURE:
are
chassis
and
monitor:
J2X. switch
to
A
±
5 for
2.0 Y
OPT
+ and 0.2 and
DRIVE
_sec. channel
SELECT
to
X OPT.
Observe
channel
Record. C.
VERIFICATION REOUIRED
switch
Record.
WITH SIDL
BEFORE
USE
DATE
21
July
64
,,JOB: DRIVE
RATE
o
Measure
the following
SELECT
switch
Equipment
ASSY:
signal
necessary
characteristics to enable 5.0
±
Pulse
width
3.0
±
Pulse
rise
Pulse
droop all grounds
all channels
to be
time
loads,
as
and
grounds,
performed.
scope
selected
by and
the
PAGE
2
OF 2
I014061-000
of channels
B
appropriate
and
channel
and
I014061-011
C, using and
DRIVE
record:
0. 5 FLsec 0.2
F_sec
NMT
0.6
v.
inputs.
jumper.
A
0. 5 vpp
NMT
DRIVE
REV: 60A06
-
amplitude
Remove are
as
JDC:04099
IFIELD)
Pulse
Reverse on
.
6
Ground Support AGC Simulator
SUBSYSTEM:
o
TEST
Observe SELECT (Leave
presence switch. jumper
of inverted
signals
Record. installed
if further
tests
)
DATE
21
July
64
JDC
APOLLO
G&N
NO.
EQUIPMENT DATA
040O9
TEST
SHEET.__.J.__ OF_I_
JOB:
DRIVE
RATE
TEST
ASSEMBLY AGC
TITLE SER
6 (FIELD)
UNDER
TEST
TEST
Simulator
NO.
H ISTORY
DATE DWG.
REV.--
MAJOR
START
END
START
END
TIME
GROUND
SUPPORT
SITE/LOCATION TOTAL ELAPSED
EQUIPMENT
NAME
SERNO.
NAME
SER.
CAL DATE
NO.-CAL DATE
APPROVEDBY
NAME/AFFILIATION
NAME/AFFILIATION
CONDUCTED BY
5.
Channel
B
delayed
from
A
2.0
6.
Channel
C
delayed
from
A
2. 0 ±
0. 2 Ftsec
7.a
Channel
B
characteristics
Amplitude Width
5.0
+
0.5
3.0
+
Rise
NMT NMT
(+X
Channel
time
C
characteristics
(+Y
5.0
±
3.0
±
Rise
NMT NMT
time
inversion,
all channels
asec v
VERIFICATION
REOUIRED
0. 5 vpp 0. 5 _zsec 0. 2 Msec 0.6 v
No
Yes
I
vpp
0. 5 _sec 0.2 0.6
Amplitude Width
Signal
_sec
OPT)
Droop 8.
0.2
OPT)
Droop 7.b
+
WITH $1DL
BEFORE
USE
DATE
Zl
July
64
JOB:
DRIVE
RATE
TEST
7 (FIELD)
Ground Support AGC Simulator
SUBSYSTEM: DESCRIPTION;
Equipment
The pulse characteristics -X OPT and -Y OPT.
Rev.
TDRR
Date
Let. A
3-9-65
and
PAGES
timing
INITIALTDRR llll9 JDC: 04100 REV: 60A06 ASSY: i014061-000
-
relationships
REVISED
of the
APPROVAL
following
D.S. PGS. 1 PAGE_]._OF_?..
A_
and
signals
1014061-011
are
checked:
REFERENCES:
NO.
JDC
D.S.
MIT
NASA
17371
All
All
_K
WR IMPORTANT:JDC's must
be
cedure
04085
completed
and
before
04086 this pro-
is performed.
IN TERVAL: Every 60 days TOOLS AND Oscilloscope MATERIAL: fier or
P6000xl0 (200 ohm,
PROCEDURE:
1.
Perform
Insert
a jumper
RST
the following
from
OPT
-X -Y
J2X
OPT OPT
Jlj Jln
2.
Ground
J2W,
3.
Ground
scope
J2X
on
Jlk,
and
Sync
5.
Set B
6.
scope
channel
on
POLARITY
delayed
Repeat
from
step
to J4e and and and
and
and
place
loads
record
the
Type
probes
M (4,
preampli Tektroni:
or equiv); 8 dummy 4 on female Dins.
loads 4 on
results.
across:
J2W Jlk Jim.
Jim.
to Simulator
chassis
and
monitor:
A
Jlj on channel Jln on channel 4.
J4A
procedure
545A,
equiv);
(Tektronix
B C.
J2X. switch
to - and
A
±
5 for
2.0 Y
OPT
0.2 and
DRIVE
_sec. channel
VERIFICA REQUIRED
SELECT
switch
to X
OPT.
Observe
channel
Record. C.
Record.
TIOH WITH SIDL BEFORE
USE DATE
21 July
64
_0B: DRIVE RATE TEST 7 {FIELD) Ground Support EquipmentSUBSYSTEM: AGC Simulator
,
.
Measure
the following
SELECT
switch
on ,
Pulse
amplitude
Pulse
width
Pulse
rise
Pulse
droop
Reverse
Remove are
loads,
as
characteristics
5.0
+
3.0
+
NMT NMT and
scope
selected
grounds,
to be performed.
ASSY:
to enable
time
all grounds
all channels
signal
as necessary
JDC:04100 60A06
by and
jumper.
on
1014061-000
channels
appropriate
B
and
channel
PAGE
A and
C,
OF
2
1014061-011
using
and
2
DRIVE
record:
0. 5 vpp 0.5
asec
0.2 _sec 0.6v.
inputs. DRIVE
the
REV:
Observe SELECT (Leave
presence switch. jumper
of inverted
signals
Record. installed
if further
tests
)
DATE
Z1 July
64
APOLLO
G aN
EQUIPMENT
DATA SHEET__L_ JOB:
DRIVE
OF_]_
RATI_
TI_$T
ASSEMBLY TITLE
NO. 041 O0 REV. _ _A I JDC INITIAL TDRR
TEST
AGC
7
UNDER
TEST
TEST
H ISTORY
DATE
Simulator
SER. NO.
1119
DWG.
REV.--
MAJOR
START
END
START
END
SITE
/ LOCATION
TIME
GROUND
SUPPORT
TOTAL
ELAPSED
EQUIPMENT
NAME
SER. SER.
NAME
NO.. CAL
DATE
CAL
DATE
NO.----
APPROVEDBY CONDUCTED
So
6. 7.
BY
NAME/AFFILIATION
NAME/AFFILIATION
2.0
+
O. 2 _sec
2.0
±
O. 2 _sec
Amplitude Width
5.0
+
0. 5 vpp
3.0
+
0.5
Rise
NMT
0.2
_sec
NMT
0.6
v
Channel
B
delayed
from
Channel Channel
C B
delayed from characteristics
A A (-X
OPT)
time
Droop Channel
C
characteristics
(-Y
OPT)
Amplitude Width
5.0
+
3.0
+
Rise
NMT NMT
time
Droop o
Signal
inversion,
all
channels
_sec
0. 5 _sec 0.2 0.6
_sec v
No
Yes
VERIFICATION REOUIRED
0. 5 vpp
WITH SIDL
BEFORE
USE
DATE
21
July
64
JOB:
PIPA
CLOCK
AND
Ground SUBSYSTEM: DESCRIPTION: The pulse PIPA CLK
A
Support
AOC
TDRR Date
TEST
Equipment
JDC:04],0I INITIALTDRR
(FIELD)
and
timing
17371
relationships
D.S.
All
PAGE_.L_OF_..?_ DS. PGS. 1
60A06
All
1041061
-(300
of the following
APPROVAL
REVISED
JDC
REV: .A 11119
ASSY:
PAGES
NO.
3-9-65
SET
Simulator
characteristics and PIPA SET.
Rev.
Let.
PIPA
and
signals
IN4f}I(_I-r)I
are
1
checked:
FERENCES:
MIT
NASA
WE
WR IMPORTANT: be
JDC's
04085
completed
and
before
04086
this pro-
e is .performed. INTERVAL: 60 TOOLS
days.
AND Oscilloscope
MATERIAL: [ier or
545A,
equiv);
Type proves
(Tektronix M (4,
preampliTektronix
I0 or equiv), 8 dummy '200 ohm, 4 on female pins.
loads 4 on
) PROCEDURE:
1.
Perform
Insert
the
a jumper
from
following
J4A
procedure
to J4e
PIPA
CLK
JIJ
PIPA
SET
JIM
2.
Ground
JIH
3.
Ground
scope
JIM JIJ
on on
scope
and
place
and
loads
record
the
results.
across:
JIH
and
JIN.
JIN.
to Simulator channel
channel on
and
and
chassis
and
monitor:
A. B.
4.
Sync
JIJ
with
5.
Observe
channel
6.
Measure
the following
B
JIH
delayed
to ground. from
signal
A
by
+
characteristics
Pulse Pulse
amplitude width
5.0
+
3.0
±
Pulse
rise
Pulse
droop
NMT NMT
time
2.0
0.5
on both
Record. channels
and
record:
vpp
0. 5 _sec 0.2 0.6
VERIFICATION REQUIRED
0. 2 _sec.
_sec v. WITH SIDL
BEFORE
USE
DATE
gl July
64
CLOCK Ground
,,IOB:PIPA SUBSYSTEM:
,
.
AGC
Reverse on both
to
loads_ be
SET TEST Equipment
JDC:04101 -
performed.
ASSY:
and Record.
groundsj
scope
and
inputs.
jumper.
REV:
A
2
PAGE
OF 2
60A06
Simulator
all grounds channels.
Remove are
AND PIPA Support
Observe
(Leave
1014061-000
presence
jumper
of
installed
and
1014061-011
inverted
if
signals
further
tests
)
DATE
Z l July
64
JDC
APOLLO G&N EQUIPMENT TEST DATA SHEET__j._I JOB:
PIPA
NO. REV.
OFJL..
CLOCK
ASSEMBLY TITLE
AGC
04101
AND
PIPA
UNDER
SET
TEST
TDRR
11119
(FIELD)
TEST
TEST
Simulator
SER. NO.
A
INITIAL
H ISTORY
DATE DWG
REV._
MAJOR
START
END
START
END
SITE/LOCATION
TIME
GROUND
SUPPORT
TOTAL
ELAPSED
EQUIPMENT
NAME
SER.
NAME
SER.
NO. CAL
DATE
CAL
DATE
NO.-
APPROVEDBY CONDUCTED
BY
NAME/AFFILIATION
5.
Channel
B delayed
6.
Channel
A characteristics
from
NAME/AFFILIATION
A
2.0
+
0.2
_sec
Amplitude Width
5.0
+
0.5
vpp
3.0
±
0. 5 _sec
Rise
NMT NMT
(PIPA
CLK)
time
Droop Channel
B characteristics
(PIPA
SET)
Amplitude Width
5.0
±
0. 5 vpp
3.0
±
0.5
Rise
NMT NMT
time
Droop 7.
0. 2 _sec 0.6 v
Signal
inversion,
all channels
Yes
VERIFICATION REQUIRED
_sec
0. 2 _sec 0.6 v
No
WITH SIDL
BEFORE
USE DATE
Z l July
64
,,lOB: EXTERNAL
TIME
Ground SUBSYSTEM: DESCRIPTION: The
Rev.
Let. A
pulse
AGC
BASE
Support
(FIELD)
INITIAL TDRR 11119 JDC: 04102 60A06 REV: A ASSY: i014061-000
-
Simulator
TDRR
and
PAGES
NO.
3-9-65
1
Equipment
characteristics
Date
TEST
17371
timing
relationships
of signal
APPROVAL
REVISED
EXT
TBI
D.S. PGS. 1 PAGE_.L_OF._z_ and
are
i014061-011
checked.
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT: must
be
JDC
's 04085
completed
and
before
04086 this pro.
cedure is performed. INTERVAL: Every
6C days.
TOOLS
AND
Oscilloscope
MATERIAL: tier or
545A, equiv);
P6000xl0 (200 ohm,
(Tektronix
Type
probes
M
preampli
(4, TektronJ
or equiv); 8 dummy 4 on female pins,
load, 4 on
pins )
PROCEDURE:
i.
Perform
Insert
a jumper
EXT
Ground
J4a
3.
Ground
scope
4.
Sync
5.
Check
6.
Measure
J4A
on
scope
to
simulator
place
loads
record
the
results.
across:
J4a
and
JIN.
chassis
and
monitor:
A
channel on
and
and
JIN.
channel
on
and
JIM
and
procedures
to J4e
J4b
SET
2.
J4b
from
TBI
PIPA
JIM
the following
channel
for coincidence the following
B. A. of the
two
signals.
Record.
signal
characteristics
Pulse Pulse
amplitude width
5.0
+
0.5
vpp
3.0
+
0.5
_sec
Pulse
rise
NMT
0.2
_sec
Pulse
droop
NMT
0.6
v.
time
VERIFICA REQUIRED
on
channel
A
and
record:
TION WITH SIDL BEFORE
USE DATE
21 July
(_4
_0B:
EXTERNAL Ground
SUBSYSTEM:
.
.
AGC
TIME BASE TEST Support Equipment Simulator
ASSY:
Reverse all grounds and both channels. Record.
scope
Remove
and
are
to be
JDC: 04102 60A06
1 {FIELD) -
loads,
grounds,
performed.
inputs.
jumper.
Observe
(Leave
I014061-000
presence
jumper
REV:
A
PAGE
and
OF
2
i014061-011
of inverted
installed
2
signals
if further
on
tests
)
DATE
21 July
64
APOLLO
JDC
G&N
EQUIPMENT DATA
TEST
SHEET__/__
JOB:
NO. REV.
OF__/_
EXTERNAL
TIME
ASSEMBLY TITLE
AGC
INITIAL BASE
UNDER
TEST
l
TEST
TEST
REV._
MAJOR
GROUND
START
END
START
END
SITE
SUPPORT
NAME
TOTAL
6.
Channel
CAL
DATE
NO.
characteristics
(EXT
No
TB])
Amplitude Width
5.0
+
3.0
±
Rise
NMT NMT
time
Droop Signal
DATE
NAME/AFFILIATION
Yes A
CAL
APPROVEDBY NAME/AFFILIATION
Coincidence
ELAPSED
NO. __
SER.
5.
ION
EQUIPMENT SER.
BY
/ LOCAT
TIME
NAME
7.
H ISTORY
DATE DWG.
CONDUCTED
11119
TDRR
(FIELD)
Simulator
SER. NO.
04102 A
inversionj
all channels
Yes
REQUIRED VERIFICATIONBEFORE WITH USE SIDL
0.5 0.5 0.2 0.6
vpp l_sec l_sec v
No
DATE
Zl July 64
JOB:
EXTERNAL
TIME Ground
SUBSYSTEM: DESCRIPTION: The
:Rev.
AGC
pulse
Equipment
INITIAL TDRR JDC: 04103 60A06
-
ASSY:
and
PAGES
NO. 3-9-65
Z (FIELD)
Simulator
TDRR
Date
TEST
Support
characteristics
iLet. A
BASE
17371
timing
relationships
REVISED
1014061-000
of signal
APPROVAL
11 119 DS. PGS. REV;. _A PAGE±OF.._
EXT
TB2
and
are
I
1014061-011
checked.
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT: ;nust
JDC's
be
cedare
04'385
co:_pleted
and
befoce
043B6 this pro-
is performed.
INTERVAL: Every 60 days. Tnr.o ^L,r_ O_cilloscope (Tektronix .^T=RIA.. J_-, , type ivlpreamp'_""'lifier or equiv); probes (4, Tektronix P6000xl0 or equiv); 8 da,m_,_/ loads (200 oh_n. 4 on female pins, 4 on male)
PROCEDURE:
i.
Perform
Insert
a jumper
EXT 3200 Ground
J3k
3.
Ground
scope
J3j JIb
5.
Sync
6.
that
rate.
Measure
fro!xl J4A
to J4e
procedure
and
and
on
and
place
loads
record
the
results.
across:
J3j and J3k Jlb and Jla. J la.
to simulator
on channel on channel
scope
Check the
following
TBZ A
2.
4.
the
and
monitor:
A B.
channel
channel
chassis
B
A. signal
is coincident
with
channel
A
but
occuring
at twice
Record. the following
signal
characteristics
VERIFICA REOUIRED
on
channel
A
and
record.
TION WITH SIDL BEFORE
USE DATE
Zl
July
64
_08:
EXTERNAL TIME BASE TEST Ground Support Equipment SUBSYSTEM: AGC Simulator
Z (FIELD} -
JDC: 04103 60A06 ASSY:
Pulse Pulse
amplitude width
5.0
±
0. 5 vpp
3.0
+
0. 5 p_sec
Pulse
rise
Pulse
droop
NM'[ _ 0. 2 ptsec NMT 0.6 v.
time
o
Reverse on both
.
Remove loads, grounds, are to be performed.)
all grounds and scope channels. Record. and
inputs.
jumper.
Observe
(Leave
I014061-000
presence
jumper
REV:
A
PAGE and
of inverted
installed
OF
Z
1014061-011
signals
if further
DATE
2
tests
Zl July
64
APOLLO
JDC
G&N
EQUIPMENT
NO. 0410_3 REV. A
TEST
DATA
SHEET._t_
JOB:
EXTERNAL
OF.._L TIME
ASSEMBLY TITLE
INITIAL BASE
TEST
UNDER
11119
2 (FIELD)
TEST
TEST
_.A..Cz.C_Ki rn :, l _ t n r"
SER. NO.
TDRR
H ISTORY
DAT E
DWG.
REV,__
MAJOR
GROUND
START
END
START
END
SITE/LOCATION
TIME
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SER.
NO._
NAME
SER.
NO._
CAL DATE
CONDUCTED
BY
APPROVEDBY NAME/AFFILIATION
5.
Coincidence
6.
Channel
A
and
NAME/AFFILIATION
rate
charactertics
Yes (EXT
No
TB2)
Amplitude Width
5.0
+
0.5
3.0
+
0. 5 FLsec
Rise
NMT NMF
time
Droop 7.
CAL DATE
Signal
inversion,
both
channels
0. 2 F_sec 0.6 v
No
Yes
REQUIRED VERIFICATIONBEFORE WITH USE SIDL
vpp
I
DATE
Zl July
64
EXTERNAL
JOB:
TIME Ground
SUBSYSTEM: DESCRIPTION: The
pulse
BASE
Support
AGC
TEST
3 (FIELD) INITIAL TDRR 11119 D.S. PGS. JDC:0410460A06 REV: A PAGE__I OF Z ASSY: 1014061-000 and 1014061-011
Equipment
-
timing
relationships
Simulator
characteristics
and
of
signals
EXT
TB3
and
800B
are
checked.
Rev. Let. A
TDRR
Date 3-9
-65
REVISED
PAGES
NO. 17 371
APPROVAL
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT: must
be
JDC's completed
cedure is INTERVAL: Every
60
04085
and
before
04086 this
pro
performed. days.
TOOLS AND Oscilloscope (Tektronix MATERIAL: 545A, Type M preamplifter or equiv); probes (4, TektroDixp6000x10 or equiv); 8 dummyloads (g00 ohm, 4 on female pins, 4 on male)
PROCEDURE:
1.
Perform
Insert
the
a jumper EXT
from
following
J4A
to
procedure
J4e
TB3
3.
.
J1U
Ground
J3i
Ground
scope
and to
simulator
on
channel
A
J1U
on
channel
B.
scope
5.
Check
6.
Measure
for
on
channel
coincidence the
record
loads
and
following
j3i
and
J1V.
chassis
and
monitor:
two
signals.
Record.
characteristics
on
A. of
the
signal
both
amplitude
5.0
+
0.
Pulse
width
3.0
+
O. 5 gsec
rise
Pulse
droop
results.
across:
Pulse Pulse
the
J1V.
J3h
Sync
place J3h
800B _°
and
and
time
I
channels
and
record.
5 vpp
NMF
0.
2 _,sec
NMT
0.
6 v.
REQUIRED VERIFICATIONBEFORE WITH USE $1DL DATE _4
_0_:
EXTERNAL
SUBSYSTEM:
.
,
TIME
Reverse all both channels. Remove are
BASE
Ground Support AGC Simulator
TEST Equipment
groands and Record.
loads,
grounds,
JDC:
3 (FIELD) -
ASSY:
scope
inputs.
and
jumper.
Observe
(Leave
04104 60A06
REV:
1014061-000
presence
jumper
PAGE
A
and
Z
ln]4ng!_0ll
of inverted
installed
?. OF
signals
if further
on
tests
to be performed.)
DATE
21
J,,ly
6a
APOLLO
EQUIPMENT DATA
JOB:
JDC
GB N
NO. 04104 REV. A
TEST
SHEET____L_
OF_l_
EXTERNAL
TIME
ASSEMBLY TITLE SER
AG¢
INITIAL BASE
UNDER
TEST
3
TEST
TEST
REV.--
MAJOR
START
END
START
END
GROUND
SUPPORT
NAME
,
SER.
BY
APPROVED
Channel
characteristics
(EXT
Rise
NMT NMT
Droop
Signal
DATE
Zl July
64
0. 5 vpp 0. 5 gsec 0. 2 FLsec 0.6 v
5.0
+
0.
5 vpp
3.0
+
0.
5 gsec
Rise
NMT NMT
time
both
CAL
NO-
Amplitude Width
inversion,
DATE
(800B)
Droop ,
+
3. 0 +
time
characteristics
CAL
No
5.0
B
NO
TB3)
Amplitude Width
Channel
ELAPSED
NAME/AFFILIATION
Yes
A
TOTAL
BY
ATION
Coincidence
/ LOCATION
EQUIPMENT SER
NAME/AFFILI
SITE
TIME
NAME
6.
H ISTORY
DATE DWG.
CONDUCTED
11119
{FIELD)
Simulator
NO.
TDRR
channels
No
Yes
VERIFICATIONBEFORE REQUIRED WITH USE $1DL
0. 2 t.tsec 0.6 v
I
DATE
JOB:
BUFFER
TESTS
(FIELD)
Ground SUBSYSTEM: DESCRIPTION: System
Support
jkGC
transformer
Date
Let. A
3-9-65
-
ASSY:
Simulator drivers
TDRR
Rev.
Equipment
INITIALTDRR JDC: 04105 60A06
are
PAGES
llll9 REV:
_A.
I014061-000
D.S. PGS 5 PAGE._L_OF_2._.
and
I014061-011
checked.
APPROVAL
REVISED
REFERENCES:
NO.
JDC
DS
MIT
NASA
17371
All
All
WK
W'R IMPORTANT: must
be
cedure
JDC's
04085
completed
and
before
04086
this pro.
is performed.
IN TERVAL: Every 60 days. TOOLS AND Oscilloscope (Tektronix" MATERIAL: 545A, Type M preampli tier or e quiv); probe (4, Tektron] P6000xl0 or equiv); 8 dummy load (200 ohm, 4 on female pins, 4 on male)
PROCEDURE: NOTE:
Perform In
this
procedural of
test
Insert
a jumper J3V.
2.
Jumper
J4h
3.
Ground
scope
separate
each from
to
J1S to
on
J3U
on
channel
J4h
should
4.
Sync
5.
Observe
scope
(coincidence Measure
of
which
should
J4A
to
J4e sure
J4i
to
and
are
testing
simulator
one
to such
be
and
be
circuit
place
chassis
and
results. In
is in
a load
order
defined
the
across is
to
followed
same
switch
Ground
the
examined.
tested
POLARITY
J1T.
record
reduce by
a list
manner. J3U
set
to
16
tests.
(+IG
ENC)
either
+ or
to
J3V.
-.
J4i.
monitor:
A B. be
J4b
monitored
with
channel not
procedure
circuits
Make and
channel
on that
of
NOTE:
J4h
NOTE:
following
the
pins
Ground
e
16
complexity,
input/output
1.
the
J4a B
to
signal
necessary).
characteristics
on
channel
A
for
all
ground. occurs
at
the
same
channel
B
rate
as
channel
A
signal
Record. of
signal
on
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
and
]
record.
0ATEZ l_!_Zat 4
JOB:
BUFFER Ground AGQ
SUBSYSTEM:
.
JDC:
TESTS (FIE_)) Support Equipment Simul_or
ASSY:
amplitude
5.0
±
Pulse
width
3.0
+ 0. 5 _sec
Pulse
rise
NMT
0. g _sec
Pulse
droop
NMT
0.6
ground
of inverted 8.
Remove
9.
Repeat signal.
time
and
signal
scope
on
input
channel
B.
the
Buffer
above
procedure
Name
for
J4h
IQI4O61-QQQ
PAGE
Z
OFz
_nd
1014061-011
0. 5 vpp
connections
v. on
J3U
and
J3V.
Observe
presence
Record.
each
of
the
following
signals.
to
J4i
to
Output
Ground
-IG
JZh
JZi
J3W
J3X
JZU
JZV
J3Y
J3Z
-MG
JZf
JZg
J3a
J3b
+OG -OG
Jlf J IP
Jig J IR
J3m J4F
J3n J4G
+ AVX
Jls
Jlu
J3F
J3G
-AVX
JZEE
JZFF
J3H
J3J
+AVY
Jlx
Jlr
J3K
J3L
-AVY
JZy J2AA
JZz JZBB
J3M J3P
J3N J3R
+XOP
J2CC JZa
J ZDD Jgb
J4j J3c
J4k J3d
-AVZ
-XOP
JIDD
JIEE
J3f
J3g
+YOP
JIFF
JIGG
J3B
J3C
-YOP
JICC
JIHH
J3D
J3E
Remove further
loads, tests
jumpers, are
to
and be
Record
for
each
Jumper
+MG
+AVZ
if
A
load.
Jumper
10.
REV:
60A06
Pulse
Reverse
04105
-
(Leave
grounds.
performed.
jumper
from
J4A
to
J4e
installed
)
DATE
21
July
64
APOLLO
JDC
GBN
EQUIPMENT
NO.
TEST
DATA
SHEET___/__
JOB:
BUFFER
REV.--_-OF 5____
TESTS
ASSEMBLY TITLE
AGC
INITIAL
UNDER
SER. NO.
TEST
TEST
H ISTORY
DATE DWG.
REV.--
MAJOR
GROUND
START
END
START
END
SUPPORT
NAME
SER.
BY
B rate Channel
Signal
-IG
ENC
5. 6.
B rate Channel
Yes
equals A rate B characteristics
+MG
ENC
,
B rate
6.
NO.
ILIAT
5.0
+
0.5
3.0
+
0. 5 btsec
Rise
NMT NMT
time
equals A rate B characteristics
CAL
DATE
Yes
No
Yes
No
0.2 0.6
vpp btsec v
5.0
+
0.5
vpp
3.0
+
0.5
btsec
Rise
NMT NMT
time
inversion
equals
DATE
ION
Amplitude Width
Channel
CAL
NO. __
Amplitude Width
inversion
Signal
ELAPSED
No
Droop 7.
TOTAL
NAME/AFF
Droop 7.
ON
APPROVEDBY NAME/AFFILIATION
5. 6.
/ LOCATI
EQUIPMENT SER.
ENC
SITE
TIME
NAME
+IG
11119
TDRR
(FIELD)
Simulator
CONDUCTED
04105
A
rate
Yes
No
Yes
No
0.2 bLsec 0.6v
B characteristics
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
DATE
21 July
64
JDC APOLLO
GS, N
EQUIPMENT
NO. 04105
TEST
DATA
SHEET
JOB:
BUFFER
z
REV._.___
OF 5.._%_ TESTS
(FIELD)
Amplitude Width
5.0
+
0.5
vpp
3.0
±
0.5
b_sec
Rise
NMT
0. g }xsec
NMT
0.6
time
Droop e
-MG
Signal
Yes
inversion
B
6.
Channel
rate
equals B
A
rate
Yes
No
characteristics
Amplitude Width
5.0
±
0.5
3.0
±
0. 5 b_sec
Rise
NMT NMT
time
Droop 7.
Signal
+OG
ENC
5. 6.
B rate Channel
inversion
equals A rate B characteristics
Yes
No
Yes
No
Amplitude Width Rise
time
Signal
-OG
ENC
5. 6.
B rate Channel
inversion
equals A rate B characteristics
vpp
0. 2 _sec 0.6 v
5.0
±
0.5
3.0
±
0. 5 _xsec
NMT NMT
Droop Yes
No
Yes
No
0.2 0.6
vpp
_sec v
Amplitude Width
5.0
±
0.5vpp
3.0
±
0. 5 _xsec
Rise
NMT NMT
time
Droop 7.
No
ENC
5.
7.
v
Signal
inversion
B
equals
Yes
No
Yes
No
0. 2 _sec 0.6 v
+&VX
5.
rate
A
rate
DATE
Zl
July
64
APOLLO
CaN
EQUIPMENT
TEST
DATA
SHEET
JOB:
BUFFER
.
3
NO.
OF___5 TESTS
Channel
B
REV.
A
(FIELD)
characteristics
Amplitude Width Rise
time
Droop .
0c I
04105
Signal
inversion
B rate Channel
equals A rate B characteristics
5.0
+
0.5
3.0
+
0. 5 _sec
vpp
NMT
0. 2 txsec
NMT
0.6
Yes
No
Yes
No
v
-&VX
5. 6.
Amplitude Width Rise
time
Signal
inversion
+
3.0
+
NMT NMT
Droop .
5.0
Yes
No
Yes
No
0.5
vpp
0. 5 Msec 0. 2 Msec 0.6 v
+AVY
e
6.
B rate Channel
equals A rate B characteristics
Amplitude Width
5.0
+
0.5
3.0
+
0. 5 bLsec
Rise
NMT NMT
time
Droop .
Signal
inversion
B rate Channel
equals A rate B characteristics
Yes
No
Yes
No
vpp
0. 2 _sec 0.6v
-AVY
5. 6.
Amplitude W idth
5.0
+
0.
5 vpp
3.0
+
0.
5 btsec
Rise
NMT NMT
time
Droop .
Signal
inversion
Yes
0. 2 bLsec 0.6 v
No
+&VZ
DATE
Zl July
64
APOLLO
GSIN
EQUIPMENT
II
TEST
DATA
SHEET__4
JOB:
BUFFER
5. 6.
INO. _041 0..0_5
OF 5__ TESTS
B rate Channel
IREV"
equals A rate B characteristics
Rise
time
inversion
5.0
+
3.0
+
NMT NMT
Droop Signal
A
(FIELD)
Amplitude Width
,
JDC
Yes
No
Yes
No
0.5
vpp
0. 5 b_sec 0. 2 b_sec 0.6 v
=AVZ
5. 6.
B rate Channel
equals A rate B characteristics Amplitude Width
Rise
time
+X
5. 6.
Signal ENG
inversion
Yes
Rise
time
e
6.
Signal
inversion
0.2 0.6
txsec v
No
5.0
+
0.5
3.0
+
0. 5 bsec
Yes
No
Yes
No
vpp
0. 2 bLsec 0.6 v
OP
B rate Channel
equals A rate B characteristics Amplitude Width
5.0
+
3.0
+
Rise
NMT NMT
time
Droop
7.
Msec
NMT NMT
Droop
ENC
vpp
0.5
equals A rate B characteristics Amplitude Width
-X
0.5
+
OP
B rate Channel
e
+
NMT NMT
Droop o
5.0 3.0
Signal
inversion
Yes
0.5
vpp
0.5
_sec
0. 2 bLsec 0.6 v
No
DATE
zl July
64
APOLLO
GS=N
EQUIPMENT DATA
SHEE
JOB:
+Y
5. 6.
TEST T._.__50F.__ 5
BUFFER
ENC
TESTS
-Y
5. 6.
equals A rate B characteristics
Yes
5.0
±
0.
3.0
±
0.5
Rise
NMT
0.2
&sec
NMT
0.6
v
Signal
time
inversion
Yes
No
Yes
No
5 vpp &sec
OP
B rate Channel
Signal
No
Amplitude Width
equals A rate B characteristics
Amplitude Width
5.0
±
0.
3.0
±
0.5
Rise
NMT NMT
time
Droop 7.
A
OP
B rate Channel
ENC
04105
REV.
(FIELD)
Droop 7.
Jo
NO.
inversion
Yes
5 vpp _sec
0. 2 Msec 0.6 v
No
DATE
zl July
64
JOB:
BURST
CONTENT Ground
SUBSYSTEM: DESCRIPTION: The
AGC
generation
Rev.
Dote
Support
INITIALTDRR 11119 D.S. PGS. 1 JDC:04106 60A06 REV: _A PAGE._I._OF Z..__... ASSY: i014061-000 and 1014061-011
Equipment
-
number
of drive
Simulator
TDRR
PAGES
NO. 3-9-65
(FIELD)
of a selected
Let. A
TESTS
17371
REVISED
pulses
in the
APPROVAL
proper
mode
is checked.
REFERENCES:
JDC
D.S.
MIT
NASA
All
.All
WK
WR JDC's
IMPORTANT: must
be
04085
completed
and
before
04086
this
pro-
:edure is performed. I N TERVAL: Every
60
TOOLS
days.
AND Oscilloscope
MATERIAL: Fief or
545A,
equiv);
P6000xl0 [200 ohm.
Type
or equiv); 4 on female
I
,
Insert
a jumper
2.
Ground
J2q.
3.
Set up
counter
4.
Set up
the
the following
from
for totaling
following
DRIVE
J4A
to J4e
count
condition
SELECT
on
.
Adjust
and
and
1 SINGLE
the
counter
record
a load
connect
J2p
panel
the
across
J2p
to counter of the
load., nn
4
model 602
or
6146
equiv)
results.
and
J2q.
input.
simulator:
- (minus)
BURST switches
place
the front
PULSES/BURST
other
and
8 dummy n]n._
Z I_RIG
POLARITY
All
procedure
model
preampli
(4, Tektroni:
(Beckman
extender
Perform
M
probes
; counter
PROCEDURE:
(Tektronix
to for
OFF
or
a count
BURST.
NORMAL. of
1 by
repeatedly
REQUIRED VERIFICATIONBEFORE WITH USE SIDL
pushing
1
SINGLE
BURST
START.
DATE
Zl
July
64
JOB:
BURST
SUBSYSTEM:
6.
7.
Rotate
PULSES/BURST
BURST
START
number
of
Remove
load,
to
be
JDC:
CONTENT TESTS (FIELD) Ground Support Equipment AGC Simulator
switch
at
each
pulses
performed.
per jumper,
burst and
ASSY:
through
position.
each
Observe selected
ground.
04106 60A06
(1(Leave
of
its
counter 256).
REV:
A
1014061-000
positions, readout
PAGE
2,
OF
and
1014061-011
depressing
SINGLE
corresponding
to
?
the
Record jumper
installed
if
further
tests
are
)
DATE
Z] July
64
JDC
APOLLO G 8,N EQUIPMENT TEST DATA
SHEETJ._
JOB:
BURST
NO. 04106 REV. A
OF__ CONTENT
ASSEMBLY TITLE
AGC
INITIAL TEST
UNDER
(FIELD)
TEST
TEST
Simulator
SER. NO.
11119
TDRR
HISTORY
DATE
DWG
REV._
MAJOR
GROUND
START
END
START
END
SITE/LOCATION
TIME
SUPPORT
TOTAL
ELAPSED
EQUIPMENT
NAME
SER.
NAME
SER.
NO. CAL
DATE
CAL
DATE
NO.-
APPROVEDBY [CONDUCTED
BY
NAME/AFFILIATION
NAME/AFF
Switch 6.
ILIAT
ION
Position 1
PULSES/BURST
1
2
2
4
4
8
8
16
16
32
32
64
64
128
128
256
256
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
DATE
Zl
July
64
JOB:
I_RIG
TEST
ROy.
generation
]
Let. i A
(FIELD)
Ground Support AGC Simulator
SUBSYSTEM: DESCRIPTION: The
1
of
a
selected
TDRR
Dote
number
PAGES
NO.
3-9-65
Equipment
17371
INITIAL TDRR 11119 D.S. PGS. l JDC: 04107 REV:, A_. PAGE .J_OF._.2_ 60A06 ASSY: I014061-000 and i014061-011
-
of
drive
REVISED
pulses
APPROVAL
in
the
proper
mode
is
checked.
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT: must
be
JDC's
04085
completed
and
before
04086
this pro
cedure is performed. INTERVAL: Every
60
TOOLS
AND
days. Oscilloscope
MATERIAL: fier
or
545A, equiv);
P6000xl0, (200 ohm,
(Tektroni:
Type
probes
or equiv), 4 on female
M
preampl
(4,
Tektroni
8 dummy loads pins, 4 on
male)
PROCEDURE:
Perform
Insert
l.
a jumper
the
from
+OG
3.
o
5.
following
J4A
procedure
to J4e
J2C
and
J2B
+X
IRIG
J2F
and
J2G
+Y
IRIG
JIX
and
JIW
+X
OPT
JIC
and
JIB
and
JIB.
Ground
J2B,
J2G,
Ground
scope
JIW,
to Simulator
J2C
on
channel
A
J2F
on
channel
B
JIX
on
channel
C
JIC
on
channel
D.
Sync
scope
Set DRIVE switch
on
J4h
SELECT
to 4,
BURST
with
and
chassis
and
place
and
loads
record
the
results.
across:
monitor:
j4i to ground.
switch
to CDU
switch
to STEADY
OG,
POLARITY BURST,
switch and
all
to other
+,
PULSES/BURST
switches
to
OFF
or
NORMAL. VERIFICA REOUIRED
TION WITH SIDL BEFORE
USE DATE
21
July
64
IRIG
TEST 1 (FIELD) Ground Support AGC Simulator
SUBSYSTEM:
6.
Observe mately
7.
8.
four every
occur
approximately Y
IRIG.
approximately
.
I0.
Observe
every
X
occur
approximately
are
to
loads, be
jumper,
four
IRIG
240
four
Z40
Observe
burst
on
channel
A.
REV:
1014061-000
Bursts
PAGE
A
and
should
2
OF2
1014061-011
occur
approxi-
Record.
every
Observe
Select
Remove
OPT.
per
msec.
X
-
ASSY:
pulses
240
Select
Select
IRIG.
CDU
Equipment
JDC:04107 60A06
msec.
four
and
burst
on
channel
B.
Bursts
should
per
burst
on
channel
C.
Bursts
should
per
burst
on
channel
D.
Bursts
should
per
Record.
I.RIG pulses
msec.
every
pulses
Record.
OPT
Z40
pulses
msec.
grounds.
Record.
(Leave
jumper
installed
if
further
tests
performed).
DATE
21
July
64
APOLLO
IJJoc I
G &N
EQUIPMENT
NO. 04107 REV. A
TEST
DATA
SHEET.__._L_.IOF±
JOB:
LEIO
TEST
1
AGC
UNDER
TEST
TEST
DWG.
REV._ MAJOR
H ISTORY
GROUND
START
END
SITE / LOCATION
START
END
TOTAL ELAPSED
TIME SUPPORT
EQUIPMENT
NAME
SER. NO. --
NAME
SER. NO.
APPROVEDBY NAME/AFFILIATION
I CONDUCTED BY
6. 7. 8.
9.
Channel Interval Channel Interval
A
pulses
240 B pulses
CAL DATE
NAME/AFF ILIAT ION
msec
4 240
C pulses
Interval
240
Channel Interval
D
4
pulses
CAL DATE
4
4
Channel
l 1 l 19
DATE
Simulator
SER. NO.
TDRR
(FIELD)
ASSEMBLY TITLE
INITIAL
240
REQUIRED VERIFICATIONBEFORE WITH USE $1DL
msec
msec
msec
DATE
21 July 64
JOB:
IRIG
TEST
2 (FIELD)
Ground SUBSYSTEM: DESCRIPTION: The
lRev. Let. A
AGC
generation
Support
number
PAGES
17371
A
LTDRR
11119
PAGE_..L_OF_._.__ D.S. PGS.
-
of drive
REVISED
I
60A06 I014061-000
of a selected
NO. 3-9-65
REV:
Simulator
TDRR
Date
Equipment
04108
pulses
APPROVAL
in the
proper
and
mode
1014061-011
is checked.
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR IMPORTANT: must
be
JDC's
04085
completed
cedure
and
before
04086
this pro
is performed.
INTERVAL: Every TOOLS
60 days. AND Oscilloscope
MATERIAL: fier
or
545A, equiv);
P6000xl0
or
](200 ohm, male);
one-
i(Minneapolis zquiv);
PROCEDURE:
I ,
Perform
Insert
a jumper
to J4e
IRIG
J2.F
and
JZG
IRIG
JIX
and
JIW
+Z
IRIG
J2 k and
J2G,
3.
Ground
scope
5.
J4A
+Y
Ground
Sync
from
+X
21
,
the following
JIW
and
on
channel
JIX
on
channel
B
J2k
on
channel
C
scope
on
On front panel BURST mode.
and
place
arid record loads
the
8 dummy
female
pins,
pushbutton
Honeywell
power
preampl
(4 Tektronix
equiv);
shot
M
supply
load,' 4 on switch
201 for
one
ED2
or
shot.
results.
across:
J2j.
j2j.
to simulator
J2F
procedure
probes
4 on
(Tektroni:
Type
chassis
and
monitor.
A
channel
A.
of Simulator
select
-X
VERIFICATION REOUIRED
IRIG,
2 pulses
per
burst,
and
SINGLE
WITH $1DL
BEFORE
USE DATE
21
July
(_4
_IOB:
IRIG
SUBSYSTEM:
6.
Depress
SINGLE
7.
Depress
J_RIG
two
pulses
8.
Depress
9.
Using <
BIAS
one-shot
Z. 5 msec,
to
push
button.
BURST pushbutton
to
loads, performed.
BIAS
pin
BIAS
switch,
J3AA two
jumper,
(use pulses
and
apply
J3FF
REQD REQD
on
START.
for
101406_-000
lamp lamp
all
three
REQD an
glow.
g
OF 2
lamp
line).
jumper
1014061-011
Record.
extinguish.
channels.
simultaneously
(Leave
and
should should
externally
return
occurring
grounds.
PAGE
A
60A06
BIAS
simultaneously
Observe
be
START.
REV:
04108
ASSY:
BURST
SINGLE
Remove are
Equipment
occurring
extinguish. Record. 10.
JDC:
TEST 2 (FIELD) Ground Support AGC Simulator
Observe
Record.
should
glow.
Record.
generated BIAS
+12
REQD on
installed
vdc,
lamp
all
three
if
m 1 _tsec should
channels.
further
tests
)
DATE
21
July
(_4
APOLLO
JDC NO. O4 ! O8 REV. A
G &N
EQUIPMENT
TEST
DATA
SHEET__i__
OF.L
JOB:
IRIG
2
TEST
ASSEMBLY TITLE
AGC
INITIAL
(FIELD) UNDER
1
TEST
TEST
HISTORY
DATE
Simulator
SER. NO.
TDRR
DWG.
REV.-MAJOR
GROUND
START
END
SITE / LOCAT ION
START
END
TOTAL ELAPSED
TIME SUPPORT
EQUIPMENT
NAME
SERNO..
NAME
SER. NO.
CAL
DATE
CAL DATE
APPROVEDBY
CONDUCTED BY
NAME/AFFILIATION
NAME/AFFILIATION
6.
Bias
REQD
7.
BIAS
REQD
lamp lamp
ON
Yes
No
OFF
Yes
No
Channel Channel
A pulses B pulses
Channel
C pulses
8.
BIAS
REQD
lamp
ON
Yes
No
9.
BIAS
REQD
lamp
OFF
Yes
No
Channel Channel
A pulses B pulses
Channel
C pulses
VERIFICATION REOUIRED
WITH BEFORE
SIDL USE
DATE
Z l July 64
_O_:
IRIG
TEST
3
Ground SUBSYSTEM: DESCRIPTION: The
Revo Let.
{FIELD} Support
AGC
INITIALTDRR JDC: 04109 60A06
-
Simulator
generation
ASSY:
of a selected
number
PAGES JDC
REVISED
TDRR
Date
Equipment
NO.
of pulses
MIT
D.S. PGS. 1 PAGE l_!_OF_.l_
1014061-000
in the proper
APPROVAL
D.S.
11119 REV: A
mode
and
i014061-011
is checked.
REFERENCES:
NASA
IMPORTANT: 04108
JDC's
should
procedure
04084,
be
04085,
completed
and
before
this
is performed.
INTERVAL:
TOOLS
60
da'rs
AND
JDC
MATERIAL: preamplifier
or
Tektronix
loads 4 on
pushbutton or
PROCEDURE:
1.
Perform
Insert
a jumper
the
from
following
J4A
to J4e and
-X
IRIG
JZK
- Y
IRIG
JZn
and
J 2m
- Z
IRIG
J2p
and
JZq.
2.
Ground
J2L,
JZm,
3.
Ground
scope
and
on
channel
A
JZn
on
channel
B
JZp
on
channel
C.
4.
Sync
5.
Repeat
scope
on
steps
channel 5 through
and
place
and
loads
545A, equiv);
equiv),
record
the
(Z00 male);
power
probes
(4,
equiv);
8
ohm,
4 on 04108;
(Honeywell supply
female one
shot
201
ED2
for one-shot.
results.
across:
J2L
chassis
and
monitor:
A. i0 of JDC
04108.
VERIFICA REOUIRED
TION WITH SIDL BEFORE
M
or JDC
switch
Type
JZq.
to simulator
JZK
operations
Oscilloscope
P6000xl0
dummy pins,
04108
(Tektronix
USE DATE
21 July
64
JDC
APOLLO G&N EQUIPMENT TEST
NO.
DATA
SHEET.J__.I OF
JOB:
BIG
TEST
I
AGC
UNDER
TDRR
DWG.
REV._
GROUND
END
START
END
SUPPORT
SER.
BY
BIAS
REQD
ION
TOTAL
ELAPSED
NO.-CAL
DATE
CAL
DATE
NO.--
APPROVEDBY NAME/AFFILIATION
REQD
/ LOCAT
EQUIPMENT
NAME
BIAS
SITE
TIME
SER.
CONDUCTED
11119
H ISTORY
START
NAME
7.
INITIAL
DATE
MAJOR
6.
A
TEST
TEST
Simulator
SER. NO.
REV.
3 (FIELD)
ASSEMBLY TITLE
041O9
lamp lamp
NAME/AFFILIATION
ON
Yes
No
OFF
Yes
No
Channel
A
Channel
B pulses
pulses
Channel
C
pulses
8.
BIAS
REQD
lamp
ON
Yes
No
9.
BIAS
REQD
lamp
OFF
Yes
No
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE DATE
21
July
64
JDC: 04110 JOB:
MISCELLANEOUS
SIMULATOR
REV:
TESTS(FIELD|INITIALTDRR
A
PAGE._]._IOF
11119
IL_ I
D.S. PGS.
|
Ground SUBSYSTEM: DESCRIPTION: The
AGC
presence
Date Let. 3-9-65
Equipment
-
Simulator of +3
vdc
TDRR
R@v.
A
Support
and
the pulse
PAGES
I
60A06
IASSY:
i014061-000
characteristics
REVISED
of signal
APPROVAL
800A
and are
i014061-0_I
checked.
REFERENCES:
NO.
JDC
D.S.
MIT
NASA
17371
All
All
WK
WR
JDC's
IMPORTANT: and
04108
should
be
this procedure INTERVAL: Every TOOLS
04084,
is
04085,
completed
befc
performed.
60 days. AND
Oscilloscope
MATERIAL: fier or
535A, equiv);
P6000xl0 (200 ohm,
Type
probes
(Tektroni: M
preampl:
(4, Tektroni
or equiv); 8 dummy 4 on female ping,
load 4 on
male)
PROCEDURE:
Perform
I.
Insert
a jumper
2.
Check
for
3.
Place
a load
4.
Ground
JIE.
5.
Ground
scope
6.
Sync
7.
Measure
.
9.
Remove
from
presence
scope
Reverse
the following
J4A
on
JID
the following
vdc
and
to simulator channel
on
pin
J4y
and
chassis
and
signal
characteristics
amplitude
5.0
+
0. 5 vpp
3.0
+
0. 5 _sec
Pulse
rise
Pulse
droop
time
ground,
the
results.
vdc
on
J3CC,
on
channel
using
scope.
Record.
JiD
A.
A.
width
load,
+3
monitor
Pulse
and
record
JIE.
Pulse
ground
and
to J4e.
of +13
across
operations
scope and
NMT
0. 2 bsec
NMT
0.6
input.
and
record:
v.
Observe
presence
of inverted
signal.
Record.
jumper. VERIFICATION REOUIRED
WITH SIDL
BEFORE
USE
1
1
DATE
21 July
64
APOLLO
JDC
G&N
EQUIPMENT
NO.
TEST
REV.
DATA
SHEET
JOB:
MISCELLANEOUS
l_J.._ OF__
ASSEMBLY TITLE
AGC
SER. NO.
SIMULATOR
UNDER
TESTS
TEST
REV._
GROUND
END
START
END
SUPPORT
SER.
Presence
check
+13
NO. __ CAL
DATE
CAL
DATE
NO._
NAME/AFF
VDC VDC A characteristics
Rise
ILIAT
ION
only Yes
No
Yes
No
(800A)
Amplitude Width
Yes
time
5.0
+
3.0
+
NMT NMT
Droop Signal
ELAPSED
APPROVEDBY NAME/AFFILIATION
Channel
TOTAL
EQUIPMENT SER.
BY
SITE/LOCATION
TIME
NAME
o
H ISTORY
START
NAME
e
11119
DATE DWG.
+3
TDRR
(FIELD)
TEST
MAJOR
_o
A
INITIAL
Simulator
CONDUCTED
04110
Yes
inversion
l
REQUIRED VERIFICATIONBEFORE WITH USE SIDL
0.5 vpp 0.5
Fsec
0. 2 b_sec 0.6 v
No
I
DATE
Zl July
64
MALFUNCTION
ANALYSIS
PRELIMINARY
JOB:
Ground SUBSYSTEM:
AGC
DESCRIPTION:
Rev.
INITIAL TDRR 11119 JDC: _0--41_3__] REV: A 60A06
-
ASSY: to
Boolean
isolate
equations
PAGES
NO.
6"
c-9-65
Equipment
procedure
TDRR
Date
Let. A
of
Support Simulator
A
utilization
FOR
TURN-ON
is
to
the
1014061-000 module
gnd
level
1014.061-011
through
the
provided.
REVISED
APPROVAL
D.S. All
JDC All
17371
malfunctions
D.S. PGS. PAGE I__OF 2,
MIT WK
REFERENCES:
NASA WR IMPORTANT: Only
for
JDC
04086
INTERVAL: TOOLS AND MATERIAL:
VTVM model
(John 803B
Fluke or
equivalent)
PROCEDURE:
1.
Isolate guide
g.
the
pertinent
in isolation
Replace
malfunction
to the
module,
using
the
table
below
as
a
analysis.
the defective
module. Signal
NASA Drawing 1014063
Origin
Equation Module
Signal
Bias Reqd (lamp on) = IRIG Bias Reset
Bias IRIG
IRIG
+3V
Reqd Bias
Sig Reset
Sheet
Location
3A21MK
5
A3
3A8AC
5
A4
la
Bias
Reset
= +3V
Relay (NASA
K2 DWG
1014098)
VERIFICA REQUIRED
TION WITH SIDL BEFORE
USE DATE
Zl July
64
MALFUNCTION _IOB:
ANALYSIS
PRELIMINARY
TURN-ON
Ground Support AGC Simulator
SUBSYSTEM:
FOR JDC:
Equipment
-
04131 60A06
ASSY:
Signal
A
I014061-000
Origin
PAGE
and
2
OF
1014061-011
NASA Drawing 1014063
Equation Module
Signal
REV:
Sheet
Location
2 IRIG
Bias
(lamp
Has
IRIG
Operated
out)
= Test RATE
Bias
Has
3A20KH
A3
2A20KH
D5
Operated
Signal No. + SBII
4 + DRIVE
Te
st No.
Signal 4
DRIVE
RATE
SBII
1B23AC
2
C2
l B20AC, IB21AC
1
B3
I
B3
2a b
DRIVE
RATE
=
F5
+ F4D
F5
i B1 2KH
C3
F4D
IAI9AC
C5
F01
2b SBII
Scaler F13A
=
F01
+
Monitor • S13
F04
+ T l
(lamp on
on)
=
I B25KH
1
C4
F04
1A24KH
1
C3
TI
3A19FD
5
C2
Scaler
Moni-
1 A4 MK
2A
1 B 18KH
3A
tor F13A S13
on
2A
DATE
21
July
64
2
MALFUNCTION JOB:
CHECK
ANALYSIS
OF
CONTINUOUS
Ground AGC
SUBSYSTEM: DESCRIPTION
A
utilization
of Boolean
Rev.
Let A
Date
FREQUENCY
OUTPUTS
Support
INITIAL
Equipment
procedure
to isolate
equations
PAGES
TDRR
17371
TDRR
11119
D.S. PGS.
-
JDC:
04132. REV:__.A PAGE_OF._._ 60A06 ASSY: I014061-000 and 1014061-011 to the module level through the
-
Simulator
NO. 3-9-65
FOR
malfunctions
4
is provided.
APPROVAL
REVISED
JDC
D.S.
MIT
All
All
WK
REFERENCES:
NASA WR
JDC
04088
IMPORTANT:
INTERVAL: TOOLS AND MATERIAL:
Counter 6146 602
(Beckman
with or
rood
extender
moq
equivalenl)
PROCEDURE:
l.
Isolate guide
2.
the in
Replace
pertinent
isolation the
defective
malfunction
to
the
using
module,
the table
a
module. NASA
Origin
Drawing
1014063
Equation Sheet
Module
Signal
(SBII) F04 +TI
as
analysis.
Signal
102.4 KC = F01 +
below
Location
IBZOAC
B3
F01
l B25KH
C4
F04
IA24KH Switch
102.4
KC
TI
VERIFICATION REQUIRED
C3 S 3
DI
WITH SIDL
BEFORE
USE
DATE
Zl July
64
MALFUNCTION 40B:
CHECK
OF
ANALYSIS FOR FREQUENCY
CONTINUOUS
Ground SUBSYSTEM:
AGC
JDC:
OUTPUTS
Support
Equipment
REV:
04132
A
PAGE
and
101406]-0]I
2
OF
4
60A06
ASSY:
Simula$or
Signal
i014061-000
Origin
NASA Drawing 1014063
Equation Signal
Module
Sheet
Location
2 25.6
KC(A)
= FZA
+ SBI
IA8AC
1
C3
F2A
1BllAC
2
D3
SBI
1B8AC
1
C3
F02
1A25KH
C4
F04
1A24KH
C3
TI
Switch
25.6
KC(A)
2a
SBI
25.6
= F02
+
KC(B)
F04
+ TI
= F2B
+ SBI
25.6 F2B
KC(B)
SBI
S-3
D1
IA8AC
B3
IA9AC
D3
IB8AC
C3
3a
SBI
: F02
+
F04
+
TI
See
2a above
+ SBI
1 2. 8 KC(A)
IA8AC
B3
F3A
IBIIAC
D2
SBI
1 B8AC
C3
4 12. 8 KC(A)
= F3A
4a
SBI
3200
= F02
+ F04
=
PPS(A)
+
F5A
TI
+ SBI
See
2a above
3200
PPS(A)
IA7AC
B3
F5A
IBI3A
C3
SBI
1 B8AC
B3
5a
SBI
= F02
+
F04
+
TI
See
2a above
DATE
21 July
64
MALFUNCTION JOB:
CHECK
SUBSYSTEM:
ANALYSIS FOR
OF CONTINUOUS Ground Support AGC Simulator
FREQUENC] JDC: 041 32
OUTPUTS Equipment
-
REV:
A
ASSY:
Signal
1014061-000
Origin
and
NASA
Equation Module
Signal
3200
PPS(B)
=
F5B
+ SBI
3200 F5B
PAGE
3
OF
4
60A06
PPS(B)
SBI
Sheet
I014061-01]
Drawing 1014063 Location
IA7AC
B3
1 B1 3AC
C3
1 B8AC
B3
6a
SBI
= F02
800
PPS(A)
+ F04
+ TI
= F7A
+ SBI
See
2a
above
800
PPS(A)
F7A
IATAC
l
A3
IB21AC,
2
C1
IAI 3AC SBI
1 B8AC
B3
IA7AC
A3
IAI3AC
CI
7a
SBI
= F02
800
PPS(B)
+
F04
+
= F7B
TI
See
2a above
+ SBI
800 F7B
PPS(B)
1BSAC B3
SBI
8a
SBI
= F02
+ F04
+ TI
See
2a
above
9 PIPA
Clock
= DRIVE
RATE
+ SBII
PIPA
Clock
3B 19AC
D3
1B23AC
C2
SBII
1 B20AC
B3
F5
1 B 1 2KH
2
C3
F4D
1A9AC
2
C5
DRIVE
RATE
9a
DRIVE
RATE
=
F5
+ F4D
9b SBII
= F01
+
F04
+ TI
See
I above DATE
21
July
04
MALFUNCTION
ANALYSIS
_IOB: CHECK
OF CONTINUOUS Ground Support
SUBSYSTEM:
AGC
FOR
FREQUENC'
OUTPUTS Equipment
JDC: 04132 60A06
-
ASSY:
Simulator
Signal
Origin
Equation Module
Signal
REV:
1014061-000
A
PAGE and
4
OF
4
1014061-011
NASA Drawing 1014063 Sheet
Location
10 PIPA
INT
RATE
PIPA
= DRIVE
DRIVE
+ SBI
INT RATE
SBI
3BITAC
D3
1BZ3AC
C2
l B8AC
B3
lOa DRIVE
RATE
= F5
+ F4D
See
9a above
See
2a above
10b SBI
= F02
+
F04
+TI
DATE
Z1 July
64
MALFUNCTION
ANALYSIS
_OB:
SCALER
TEST
Ground Support AGC Simulator
SUBSYSTEM: DESCRIPTION: utilization
Rev. Let.
Date
A
3-9-65
A
04134
INITIAL
to isolate
I malfunctions
REV:
TDRR
A
11119
60A06 1014061-000
to the
module
PAGE l__OF._.3..3 D.S. PGS.
and
level
101406]-011
through
the
is provided.
REVISED
JDC
APPROVAL
D.S. All
All
17371
JDC:
IASSY
PAGES
NO.
AND
1
equations
TDRR
CLOCK
Equipment
procedure
of Boolean
FOR
MIT WK
REFERENCES:
NASA VTR
JDC
04090
_RTANT:
INTERVAL: AND MATERIAL: fier,
ohm,
(Tektronix
535A,
or equiv);
P60000xl0 (200
_cope
or
Type
M
probes equiv);
4 on
preampli-
(4,
Tektronix
8 dummy
female
i_ins,4
loads on
male
PROCEDURE: I.
Isolate in
2.
the
pertinent
isolation
Replace
malfunction
to the
module,
using
the table
the
defective
a guide
module.
Origin
NASA Drawing i014063
Equation Module
Signal
KC(A)
as
analysis.
Signal
25.6
below
= F2A
+ SBI
Sheet
Location
1A8AC
C3
F2A
1BI
D3
SBI
1 B8AC
C3
F02
IA25KH
C4
F04 TI
IA24KH Switch
25.6
KC(A)
IAC
]a
SBI
= F02
+ F04
+ TI
VERIFICATION REOUIRED
WITH SIDL
BEFORE
USE
1
S-3
C3 D1
DATE
Z1 July
64
MALFUNCTION jOB:
ANALYSIS
AND Ground
SUBSYSTEM:
AGC
SCALER Support
FOR
CLOCK JDC:
TEST 1 Equipment
041
34
REV:
ASSY:
Simulator
Signal
1014061-000
Mo
Signal
CDU
SET
[ +DRIVE
= OG
(DDR
INH)]
SBR
CDU
1 + EXT
No.
+OG OG
CDU
SET
C DU
(DDR
2.
and
1014061-011
OF
SBR
Location
4
3AC S- I I
2BI7AC
D3
4
C5
3
B3
B5
1 + EXT
INH)] +DRIVE DDR
2AI
Sheet
dul e
Switch
[ +DRIVE
i
PAGE
NASA Drawing 1014063
Origin
Equation
+OG
A
60A06
-
I No.
l
Switch
S-I 0
3
Switch
S-4
3
C5
2AI4AC
3
A4
2a
SBR
No.
+ SBII
I = DRIVE + Burst
RATE
IB23AC
2
C2
1B20AC
1
B3
3AI
IAC
5
C2
F5
i B 1 2KH
2
C3
F4D
IA9AC
2
C5
F01
IB25KH
1
C4
DRIVE
RATE
SBII
Gate
Burst
Gate
2a. i DRIVE
2a.
= F5
+ F4D
2 SBII
2a.
RATE
= F01
+
F04
+ TI
F04
IA24KH
TI
Switch
S-
1
C3
5
D1
3 Burst
Gate
= BURST
+ END
BURST
3A10AC
5
D2
BURST
3A11AC
5
C2
Burst
Switch
S-8
5
D5
Switch
S-8
5
D5
BURST END
2a. 3. 1 BURST
= Single
+ Steady
Burst
Burst
Single Steady
Burst
DATE
21 July
64
MALFUNCTION CLOCK
_OB:
Ground SUBSYSTEM:
ANALYSIS
AND
AGC
SCALER Support
FOR
TEST
I
Equipment
JDC: -
Simulator
04134 60A06
ASSY:
Signal
102.4
512
KPPS
KC
= C2
= F01
+ TI
+ F04
+ TI
A
i014061-000
PAGE3
and
Module
Sheet
Location
1B20AC
B3
1B25KH
C4
F04
1A24KH
C3
TI
Switch
512
KC
KPPS
3AI
3
i014061-0]l
F01
102.4
OF
NASA Drawing 1014063
Origin
Equation Signal
REV:
S-3
D1
C3
IAC
C2
I B27KH
TI
Switch
D2 D]
S-3
DATE
21 July
64
MALFUNCTION JOB:
ANALYSIS
Ground SUBSYSTEM:
AGC
DESCRIPTION:
Support
BUFFER
Equipment
procedure
ASSY' to isolate
of Boolean
Rev. Let.
TDRR NO.
PAGES
17371
All
Date 3-9-65
INITIAL 0__44149 TDRR JDC:
-
Simulator
A
utilization
A
FOR
TESTS
equations
malfunctions
to the
11119 Am REV:
1014061-000
module
level
D.S, PGS. -PAGEfl.L_OF.3_
and
i014061-011
through
the
is provided.
REVISED
JDC
APPROVAL MIT WK
D.S.
REFERENCES:
JDC
04105
NASA WR IMPORTANT:
INTERVAL: TOOLS AND Oscilloscope (Tektronix MATERIAL: 535A, Type M preamplJ fier or equiv); probes (4, Tektron P6000xl0 or equiv); 8 dummy load (200 ohm, 4 on female pins, 4 on male),
PR
OC E DURE
Isolate
I.
guide
,
3.
the
pertinent
in isolation
Replace
Use
:
the defective
Table
A
as
malfunction
to the module,
using
the
table
below
as
a
analysis. module.
a guide
in isolating
the buffer
VERIFICATION REQUIRED
modules.
WITH SIDL
BEFORE
USE
DATE
MALFUNCTION
ANALYSIS
FOR
BUFFER JDC: 04149
_OB: TESTS SUBSYSTEM:
Ground
Support
Equipment
A$SY:
Table
AGC
REV:
A
+IG -IG
CDU CDU
s Location
ENC
IB6DA
and
IB4CR
1
B4
ENC
IB6DA
and
IB4CR
1
B4
IA22CR
1
B4
IA22CR
CDU
ENC
IA26DA
-MG
CDU
ENC
IA26DA
+OG
CDU
ENC
IB5DA
-OG
CDU
ENC
IB5DA
+AVX
Drawing
Sheet
+MG
PIPA
2B27DA
and
1
B4
and
IB4CR
1
B4
and
IB4CR
1
B4
2A27CR
3
D2 D2
and
and
-AVX
PIPA
2B27DA
and
2A27CR
3
+AVY
PIPA
3B21DA
and
3B20CR
6
C4
PIPA
3B21DA
and
3B20CR
6
C4 C4
-AVY +AVZ
PIPA
3B22DA
and
3B20CR
6
-AVZ
PIPA
3B22DA
and
3B20CR
6
C4
and
IA22CK
i
A4
+X
OPT
ENC
IB22DA
-X
OPT
ENC
IB22DA
and
IA22CR
I
A4
ENC
2A26DA
and
2A27CR
3
D2
2A27CR
3
D2
+Y -Y
OPT OPT
ENC
2A26DA
OF
A
Module
Name
3
Simulator
NASA Buffer
PAGE
and
DATE
3
MALFUNCTION _OB:
ANALYSIS FOR BUFFER JDC:
TESTS
SUBSYSTEM:Ground
Support
AGC
ASSY:
Equipment
Signal
REV:
04149
A
PAGE
2
OF
Simulator
NASA
Origin
Drawing 1014063
Equation
PDR
(J4-h
=SBR
No.
and
J4-i)
Signal
Module
PDR
2.AI 8AC
SBR
l (±DRIVE)
No.
1
2AI4AC Switch
± DRIVE
S10
Sheet
Location
3
B3
3
A4
3
B5
la
Single =DRIVE Gate
C2
3Al
C2
DRIVE
+ SBII
SBII
IB20AC
B3
F5 "F4D
IBI 2KH
C3
IA9AC
C5
F01
1B25KH
C4
F04
1A24KH
C3
TI
Switch
BURST
3AIOAC
D2
3A1
C2
Bur
RATE
1B23AC
Burst Reset No. RATE + Burst
st Gate
1AC
la.l DRIVE
RATE
= F5
+ F4D
la. 2 SBII
= F01
+ F04
+ Tl
D1
S- 3
la. 3 Burst
Gate
= BURST
+ END
END
BURST
BURST
2KH
la. 3. 1 BURST +
= Single
Steady
Burst
Burst
Single Steady
Burst Burst
Switch Switch
S- 8
D5
S- 8
D5
DATE
3
JOB:
512-KC CLOCK CALIBRATION INITIALTDRR 11119 D.S. PGS. 1 JDC: 04154 REV: _A PAGE_]._OF._..I_ 60A06 ASSY: I014061-000 and 1014061-011
Ground Support Equipment SUBSYSTEM: DESCRIPTION:
Rev.
"_'.4
AGC
Simulator
The
512-kc
TDRR Date
PAGES
NO.
.Let.i A 3 -9 -65
clock
in the
AGC
REVISED
Simulator
APPROVAL
REFERENCES:
JDC
D.S.
MIT
NASA
All
All
WK
WR
17371
is calibrated.
ND
JDC
1021002 04087
IMPORTANT:
INTERVAL: TOOLS AND MATERIAL:
AGC Calibration Systen coaxial cable with BNC connectors
04062
PROCEDURE: 1.
Perform
g.
Lift up
3.
JDC Logic
04062. Plate
oscillator
(IB28BJ).
Using
the
coaxial
front
panel
Calibration
Assembly
cable
with
to COMPUTER System.
connectors
SIGNAL
Turn the tuning adjustment the counter. Record.
5.
Replace
screw
BNC
remove
on the
the
screw
on the top
connect Control
CLOCK
and
of the
SYNC
Interface
on the
Panel
simulator
of the
AGC
Record.
4.
the
l and
and
on
the
disconnect
oscillator
the
VERIFICATION REOUIRED
AGC
to read
Calibration
5]Z000.00
+
0. 05
cps
on
System.
WITH SIDL
BEFORE
USE
DATE
Zl July
64
APOLLO
EQUIPMENT DATA
I INO.
G 8_N TEST
SHEET__]._
JOB:
51z-KC
IREV._A----
OF_L_
CLOCK
ASSEMBLY TITLE
[INITIAL
TDRR
CALIBRATION UNDER
TEST
TEST
HISTORY
DATE
AC, C. _im,;]_t-nr
SER. NO.
JDC 04154
REV._
DWG.
MAJOR
GROUND
START
END
START
END
SITE / LOCATION
TIME
SUPPORT
TOTAL ELAPSED
EQUIPMENT
NAME
SER. NO.__
NAME
SER. NO.-
NAME/AFFILIAT
NAME/AFFILIATION
CLOCK
4.
Oscillator
CAL DATE
APPROVEDBY
CONDUCTED BY
3.
CAL DATE
SYNC
connected
to COMPUTER
ION
SIGNAL
frequency
512000.00 0.05
VERIFICATION
±
cps
WITH SIDL
REOUIRED BEFORE USE
DATE
Zl July 64
JOB:
AGC
SIMULATOR Ground
SUBSYSTEM: DESCRIPTION: timing
Rev. Let.
AGC
CHECKOUT Support
INFORMATION
INITIAL TDRR JDC: 0423.___4 60A06
-
Equipment
ASSY:
Simulator
Contains
AGC
Simulator
PAGES JDC
REVISED D.S.
checkout
flowgram,
19122 REV:_..=_.-
I014061-000 typical
D.S. PGS. PAGE._/_OF
and
4.
I014061-011
waveform,
and
diagram.
Date
TDRR NO.
REFERENCES:
APPROVAL MIT NASA
IMPORTANT:
INTERVAL: AND MATERIAL:
This the form.
AGC
JDC
contains
Simulator Figure
three checkout
3
is
a timing
figures
to
aid
flowgram.
in
AGC
Figure
Simulator
2 is
an
illustration
checkout.
Figure of
a typical
1 is wave-
diagram.
VERIFICATION REQUIRED
WITH SIDL
BEFORE
USE
DATE
9 March
65
408:
AGC SIMULATOR CHECKOUT INFORMATION Ground
SUBSYSTEM:
AGC
Support
Equipment
JDC: 04234 60A06
-
ASSY: 1014061-000
Simulator
-_-_ O
REV:
and
PAGE
2
OF
4 ,
I014061-01_
_ooo-
w
O_OO
-
OO_
_oo _ o_o
__-_5
oooo
oo88
:_88
0
_
o 0
o
6 0
.r-i
o <
_0_-_
i
"_
OOO
i
OO
_o_ :D_-)
DATE
9.March
65
AGC SIMULATOR CHECKOUT JOB: INFORMA TION Ground Support Equipment -
JDC: 04234
SUBSYSTEM:
ASSY:
AGC
Simulator
REV:
-
PAGE
3
OF
=t
_nl
]
60A06 I014061-000
and
1fl14fl_l
(NEGLECT)
90%
1
AMPLITUDE
PW
I t E I I I 10%
I1
_1-
T F -_
(NEGLFCT) 03S_
Figure
2.
Typical
AGC
Simulator
Waveform
DATE9
March
65
AGC JOB:
SIMULATOR
INFOR
MA Ground
SUBSYSTEM:
AQ¢
CHECKOUT JDC:04234
TION Support
REV:
-
PAGE
4
0F4
60A06
Equipment ASSY:
Simulator
101406]-000
and
1014061-0]I
El E
=o .9
I
r-r-r--
E .,.-4
C_
rE
.,-4
E F_
E]
I-L_
°,-_
E
El I I E
E
H 0
H
_
,(
_
t_
_
k'e
m_
J
_,
om
J,_
w
i%1
ee 04 t_.
_p b-
_r) tL
DATE
9 March
65
_0B:
PRELIMINARY
TURN-ON
(FIELD) JDC: INITIAL 04466 TDRR
SUB,_YSTEM: DESCRIPTION:
Ground
Preliminary
front
Rev. Let.
Date
Support
panel
TDRR
Equipment
and
power
PAGES
NO.
ASSY:
supply
REVISED
JDC
AGC
PAGE._LOF._.2.2 D.S. PGS. 2
Simulator
1014061-011
checks
APPROVAL
DS.
REV: 16306 :
MIT
3ES:
NASA ND
1014251
ND
I020202
IMPORTANT:
JDC
before
04085
this
must
procedure
be
corn-
is
per-
INTERVAL:
TOOLS
PROCEDURE:
Perform
1.
Energize
2.
Set
LOGIC
LOGIC .
Press
115
vac
to
POWER
POWER IRIG
the
BIAS
SCALER
TEST
5.
Set
TIMING
INHIBIT
ND
switch
lamp
switch should
d-c
ON. to
REQD SCALER
no
assembly)
should
to
should go
TIMING
ON
lamp
REQUIRED
ON
position.
lamp
USE
glows.
INHIBIT (refer
to
should lamp ND
WITH SIDL
BEFORE
Model
glow.
1014251):
VERIFICATION
Fluke
equivalent).
out.
OPERATING
continuity
(John or
POWER
lamp
TEST
Read
results.
the
supply
position,
off.
record
REQD LAMP
VTVM 803B
STANDBY
BIAS
INHIBIT go
that power
glow. BIAS
to
and
check
(on
should
switch
TEST
procedure and
pushbutton.
Set
SCALER
Simulator ON
ON
4.
glow.
following
AND
MATERIAL:
DATE
blink. should
1020202
and
JOB:
PRELIMINARY
SUBSYSTEM:
o
Ground
Jlv
$1w
J lv
J4n
J4m
J4n
J4m
5 ]w TIMING
9.
TIMING
INHIBIT TEST
10.
switch lamp
to
should
go
OPERATING
continuity
NORMAL
(refer
to
should
1020202
ND
Jlw
31 v
J4n
34m
J4n
J4m
J lw POWER
ON ON
a jumper
SCALER
Using
TEST
13.0
±
from
switch
J3e to
d-c go
15 0.65
vdc vdc
at
3-volt at
13-volt
power
supply
assembly)
to
OFF
position.
off.
to
34BB.
LOGIC
POWER
ON
lamp
should
OFF.
test
OF
1014061-011
measure 0.
±
(on
should
wire
VTVM, 3.0
switch
lamp
Simulator
Z
1014251):
Jlv
POWER
PAGE
blink.
and
To
LOGIC
AGC
-
out.
lamp ND
REV:
position.
From
Connect Set
INHIBIT
SCALER
LOGIC o
ASSY:
Equipment
Support
04466
To
Return
Set
JDC:
(FIELD)
From
Read
,
TURN-ON
points points
on on
Power
Power
Supply Supply
Assembly. Assembly.
DATE
glow.
Z.
1
APOLLO GSN EQUIPMENT TEST
I NO.
OF.__.z
PRELIMINARY
AGC
I INITIAL
TURN-ON
ASSEMBLY TITLE
04466
IREV.--_---
DATA SHEET__L_ JOB:
JDC
TEST
TEST
DWG.
START
END
START
END
TIME
REV._
MAJOR
HISTORY
DATE
1014061-011
SER. NO.
GROUND
SUPPORT
SITE/LOCATION TOTAL ELAPSED
EQUIPMENT
NAME
SER.
NO.
NAME
SER.
NO.
:ONDUCTED
CAL DATE CAL DATE
APPROVEDBY
BY
NAME/AFFILIATION
NAME/AFFILIATION
Verify
I.
STANDBY
2.
LOGIC
POWER
ON
BIAS
REQD
3.
BIAS
4.
SCALER
TEST
5.
TIMING
INHIBIT
REQD
on
lamp
on
lamp
out OPERATING
SCALER
TEST
TIMING
LOGIC
lamp
switch
INHIBIT
blinks
to INHIBIT
lamp lamp
continuity
on off
Jlv to Jlw 5 1v to J4n
INHIBIT
J4m
to J4n
J4m
to J lw
switch
to NORMAL
TIMING
INHIBIT
lamp
SCALER
TEST
OPERATING
Continuity
7.
on
lamp
TIMING
No
6.
lamp
POWER POWER
Jlv Jlv
to to
out lamp
blinks
$1w J4n
J4m
to
J4n
J4m
to
J lw
POWER POWER
ON
lamp
16306
(FIELD)
UNDER
Simulator
TDRR
off
REQUIRED VERIFICATIONBEFORE WITH USE SIDI..
DAT E
APOLLO GSN EQUIPMENT TEST DATA SHEET JOB:
ir
z OF_2._z
PRELIMINARY
TURN-ON
NO. 04466 dDC REV. -
(FIELD)
Verify 8.
LOGIC
POWER
POWER 9.
SCALER
10.
Voltages
TEST
ON
lamp switch
on OFF
3 vdc
3.0
13 vdc
13.0
DATE
•
0.15
vdc
± 0.65
vdc
