LM 0RIENTATI ON COURSE NO. 30005-012 For Training Purposes ...
73
LM 0RIENTATI ON COURSE NO. 30005-012 For Training Purposes Only DATE: April 12, 1966 REVISED: November 1966 Prepared by: Product Support Department
Transcript of LM 0RIENTATI ON COURSE NO. 30005-012 For Training Purposes ...
LM
0RIENTATI ON
COURSE NO. 30005-012
For Training Purposes Only
DATE: April 12, 1966
REVISED: November 1966
Prepared by:
Product Support Department
LESSON PLAN
I. Introduction i__ _ -
A. Objective
To provide the student with an orientation of the LM spacecraft.Included will be a brief functional description of each LM opera-
tional subsystems to a block diagram level with emphasis on the
major signal flow paths.
B. Motivation
!n order to provide adequate operational support to the ApolloMission one must have a basic functional knowledge of LM opera-
tional subsystems and the associated subsystem interfaces.
II. Presentation
A. Film - Apollo Lunar Mission Profile
B. IM Basic Design Concept
i. Ascent Stage
a. Cabin area
b. Aft equipment bay
2. Descent Stage
3. Summary
C. Crew Station
i. Controls and Display Panels
D. Propulsion Subsystem
i. General Configuration
a. Descent
b. Ascent
c. Reaction Control
2. Descent Propulsion
a. Propellant Pressurization
b. Propellant Feed
c. Engine Control
3. Ascent Propulsion
a. Propellant Pressurization
b. Propellant Feedc. Thrust Control
d. RCS Crossfeed
4. Reaction Control
a. Cluster Configurationb. Attitude and Translational Control
c. Propellant Pressurization
d. Propellant Feed
5. Controls and Displays
6. S_Immary
E. Environmental Control Subsystem
1. Atmosphere Revitalization Section
a. Pressure Schedules
b. Closed Suit Loop Operation
c. Open Suit Loop Operation
2. Oxygen Supply and Cabin Pressure Control Section
a. Tankageb. Descent Feed
c. Ascent Feed
3. Water Management Section
a. Tankageb. Descent Feed
c. Ascent Feed
4. Heat Transport Section
a. Primary Loop Operationb. Secondary Loop Operation
5. Controls and Displays
6. S1]_ary
F. Electrical Power Subsystem
i. General Configuration
a. Ascent Stage
b. Descent Stage
2. System Functional Description
a. Batteries
b. Electrical Control Assembly (ECA)
c. Relay Junction Box (RJB)
d. Deadface Relay Box (DFRB)e. Inverters
f. Electroexplosive Devices
3- Controls and Displays
4, S1 ]T_ml a_y
G. Guidance, Navigation, and Control Subsystem --_/ /}'i__
1. System Concept
2. Functional Description
a. Hand Controllers
b. Primary Guidance and Navigation Section _PGNS )
c. Abort Guidance Section (AGS)
d. Control Electronics Section (CES)
3. Controls and Displays
4. S11_ary
H • Instrumentation
1. System Concept
2. Functi9nal Description
a. Signal Conditioning Electronics Assembly (SCEA)
b. Caution and Warning Electronics Assembly (CWEA)c. Pulse Code Modulation Timing Electronics
Assembly (PCMTEA)
d. Data Storage Electronics Assembly (DSEA)
3. Controls and Displays
I • Communications
i. Operational Capabilities
a. IN FLIGHT
b. LUNAR STAY
2. System Concept
3. Functional Description
a. SIGNAL PROCESSOR ASSEMBLY
b. S-Band
c. VHF
4. Controls and Displays
J. Final S1_ary
LM ORIENTATION
Abbreviation Document
AEA Abort Electronics Assembly
AGS Abort Guidance Section
AOT Alignment Optical Telescope
ARS Atmospheric Revitalization Section
ASA Abort Sensor Assembly
ATCA Attitude and Translation Control Assembly
CES Control Electronic Section
CM CommandModule
CSM Command and Service Module
C/W Caut ion/Warning
CWEA Caution and Warning Electronics Assembly
DECA Descent Engine Control Assembly
DEDA Data Entry and Display Assembly
DFRB Deadface Relay Box
DSEA Data Storage Electronics Assembly
DSKY Display and Keyboard
ECA Electric Control Assembly
ECS Environmental Control Subsystem
EPS Electrical Power Subsystem
EVA Extravehicular Astronaut
GN&C Guidance, Navigation and Control Subsystem
G0X Gaseous Oxygen
He Helium
H20 Water
}ITS Heat Transport Section
IMU Inertial Measuring Unit
LM LunarModule
LGC LM Guidance Computer
LR LandingRadar
LUT Launch Umbilical Tower
MSC Marmed Spacecraft Center (Houston)
MSFN Manned Space Flight Network
0SCPS Oxygen Supply and Cabin Pressure Section
Ox Oxidizer
PCM Pulse Code Modulation
PCM_EA Pulse Code Modulation and Timing Electronics Assembly
PGNS Primary Guidance and Navigation Section
PISS Portable Life Support System
RCS Reaction Control Subsystem
RJB Relay Junction Box
RR RendezvousRadar
S & C Stabilization and Control
SCA Signal Conditioner Assembly
SCEA Signal Conditioning Electronics Assembly
SM ServiceModule
TEA Timing Electronics Assembly
TV Television
VHY Very High Frequency (30-300 mc)
W_v_ Water Management Section
This does not constitute a complete list of LM abbreviations.
Grumman document LLI-790-1 may be consulted for abbreviations not listedhere.
VHFANTENNA(2)
S-BANDSTEERABLE ASCENTSTAGEANTENNA DOCKING EVA
HATCH ANTENNARENDEZVOUS DOCKINGTARGETRADARANTENNA
AFTEQUIPMENTBAY
OVERHEADDOCKINGWlNDOW < -
S-BAND RCSINFLIGHT THRUSTERANTENNA(2) ASSEMBLY
iNGRESS/ RCS NOZZLEEGRESSHATCH
LANDINGGEAR
(+Z) '_
JEGRESSPLATFORM DESCENTENGINE DESCENT _/SKIRT STAGE
¥
LM VEHICLE T3ooo-,_DEC 66_
:::::::::::::;:_
i i iiiiiiiiiliiiiiiiiiiiiilii!i¸ _!$i:i :!$
LM_;SLAINTERFACE
J•-_.,.a_ 4" e#'.._,_
k\
_!iil!!ili!i_il::::::::::::::::::::
iiiii!!i!i _:,iiiiii_i i_
[LM StuBBOOSTERINTERFACEIT_005-14
,_ " ,. -_ ---- DEC 66
+ X 233.,'5 I(REF) ./ _ -Z27(REF)
+X215
(REF ) + Z27 (REF)
(_ EQUIPMENT LOCATIONSASCENT STAGE-R/H SIDE T3ooo5-32NOV 66
-.-.1 /o,sco.._CTS
%DESCENTOXYGENTANK
..__ -÷ZZT(REF)
c_ .S.',j,.
----eXl_ (REF)
----'_XI31(REF)
QUAD 4
DESCENT STAGEEQUIPMENT LOCATIONS
NOv 66
99^ON[39VLS1N39S3QI_171 @I-_O00EI
_t
/:
(Z÷)"_,
\
_2
LM DISPLAYS AND CONTROLS T_ooo_-_DEC 66
\
LM TO MSFN CREW, CABIN I
ELECTRONICS__I "_SUBSYSTEMS AND SM a EQUIPMENT] tl
STATUS VOICE AND THERMALINFORMATION TELEMETRY MANAGEMENT CONDITIONED
J I [ °'ENVIRONMENTAL
INSTRUMENTATION ,TM DATA 1 COMMUNICATIONS CONTROL/
l INSTRUMENTATION CONTROL IVOICEINSTRUMENTATION DISPLAY
EPS CONTROL J CREW, _ ECSCONTROLCOMMANDS
1 STATUSOATA 7 CONTROLS _ STATUS INFORMATION
AND DISPLAYS MANUAL ENGINE COMMANDSSTATUS DATA
STATU#SDATACONTROL COMMANDS
ELECTRICAL t PROPULSIONAND REACTIONPOWER GUIDANCE, CONTROL
NAVIGATION
I I AND CONTROL TDC AC JPOWER POWER
_, ENGINE CONTROL COMMANDSLM
SUBSYSTEMS I LM OPERATIONAL BLOCK DIAGRAM] TSOOOS-29NOV66
/ ,l
SQU_B
Ho TANK DISKS
__ FUEL He [ I----J I
H_ _ HEAT EXCHANGERI I--_ I_J.VE '"_ (CHANGER\ _ _ J
VALVIES FILTER
P_.SSUREREGULATORS
f
NEUTRALIZERS QUAO #
CHECK "1-',_;i"_ _ - VALVES
SQUIB " '_f<'_'" _:_
ox,_zE_ ox,o h_ - _'_ _ _
TRIM ORIFICE TRIM ORIFICE
FILTER _ILTER
T 50005 - 154
I DESCENTPROPULSIONISCHEMATIC NOV66
FUEL
FILTER FILTER(FUEL) (OXIDIZER)
TRIM TRIMORIFICE ORIFICE
TO ACTUATOR\ ISOLATION VALVES
TO TORCS RCS
d
t
(J f " _' _ [.... IASCENT PROPELLANT SYSTEMI
+X
VHFANTENNA(2)
ASCENTSTAGES-BANDSTEERABLE DOCKING EVA
AN1T..NNA _ HATCH ITENNA
DOCKINGTARGETRENDEZVOUSRADAR
ANTENNA AFTEQUIPMENTBAY
OVERHEADDOCKINGWINDOW <
S-BAND RCSPITCH INFLIGHT THRUSIER
ANI_NNA(21 ASSEMBLY
RCSNOZZLEINGRESS/EGRESS
HATCH LANDINGGEAR
+Z ROLL
DESCENTEGRESSPLA_ORM DESCENTENGINE STAGESKIRT
I LUNAR MODULE I T30oo5-161AXES NOVee
HELIUM PRESSURE SYSTEM"A"REOULATINGPACKAOE TANKAGE
SYSTEM"B"
TANKAGE
THRUSTCHAMBER __
ISOLATION VALVES BLADDER ,"_ "'h
TANK ii!_X_/THRUST CHAMBER ">-
ASSEMBLY
_,' ._- _i"_
® i /_ ®@ ®
® ( (9 '2 r /
/< (!)MAIN SHUTOFF RCS MANIFOLD
VALVES CROSSFEED AND
ASCENT ENGINE +X
PROPELLANT TRANSFER -Z -Y
VALVES _ _ _+y +Z
-X
SYSTEM"A" FUELLINE A,.'< ESOXIDIZER LINE ORIENTATION
_F ---- HELIUMSYSTEM Jl_Jl
IRCSINSTALLATIONI T30005-149NOV66
IFILTER
OXIDIZER "A" _ I
u,OX,O,ZER"B"II __L_ _ATERN SHUT-OFF VALVE ]
|1 C.A"BER I -ll ;
ISOLATION I
I I_LLAVALVES I
c _ _--_--__FILTER
SGUIB ,t__ "TANK
BURST _ _-= VALVE
;DISK _ -BLADDER
FUEL"A"RELIEF _HE A) v SYSTEM "A"
ASCENTOX tt:_jPROPULSION INTERCONNECT OXIDIZE R "A" VALVE
INTERCONNECT VALVES FUEL "B" _HE"'_' SYSTEM "B"
__. OXIDIZER "B"
PROPELLANTFILTERS _
,, F-_1I iII
T3000S- 151
REACTION CONTROL NOV,BSUBSYSTEM SCHEMATIC
L,<.... r-. I/,: s,(.;,.l_,r .I-,
/ \• llll,--_i[ _- i III_.... _I..... ,
lllL_o-Jl ,- ]lli-,,,,, II_1[ 11 '" 011 II
\.,,.-,,-. ,_,,,,-.331 -8-_11\[toeose3T}(Is_ss]eo} _e
T_T r£1W P_£ss
io ..-,.,--' t X-PC411TEll
I I r'"r "r t',,'r"_
T/W O01D(XaIcr
_;: Jg/'//n//_/M//////_z/////////._//_
ENT Ht _ime_ _ENG_M X-TRAMSLBALCW.
. 4_. . [] TEIdWPI_SSIdON
o_-" -o
[ PANEL I J "rsooos-_'-z- DEC 66
i PANEL1TI T30005-160DEC 66
ENVIRONMENTAL CONTROLSUBSYSTEM
(ECS)
ATMOSPHERE WATER HEATREVITALIZATION MANAGEMENT TRANSPORT
SECTION SECTION SECTION(ARS) (WMS) (HTS)
II LM ECS BASIC BLOCK DIAGRAM T3oooH,FEB. 68
323
CABINPRESSURESWITCH I
PRESSURE ISENSING TO" - - FROM SUIT SUIT I
LOOP LOOP L. OVERBOARD VACUUMPRESSURIZED AREA
_. CABIN PRESSURE
PLSS 02 ____ RELIEFAND
DISCONNECT r _ DUMP VALVES .| ,A, --
I ---J IJ FILTER -- OXYGEN --iI TO__ CABIN
_- DE.NO ' _'-_!I PLSS REGULATORS I|
I SERVICE . I-- .... |I VALVE CABIN Ij _ REPRESSAND EMERG
,I ._-_--. _,- O2VALVE ,
I I, ,I I IJI _" I _, ,l _sc NO1L_" OESC. ASCNO2 |J FEED FEED FEED _ " i _'I _ _ I _'
a, /I
FILTER M 0 2 MODULE FILTER FILTER _ j
FLEX /' _' ._
LINES INTERSTAGE _ "- -_...... ;CONNECT : "_
ASCENT STAGE __ _ ",_. r,DESCENT STAGE" \ . r_
BURST DIAPHRAGM i_
RELIEF VALVE -- "_i
ISSURE REGULATOR " ;"
BYPASS._J1
/-GSE I
(J , DISCONNECT "., _i ' :
"_ -:- '_ ,t _ DESCENT / _" a---__, TANK 'v" _ ,
_., . ._ __ -_ _
OXYGENSUPPLYANDCABINPRESSUREI _" "'_ _ 'CONTROLSECTIONSCHEMATIC "'%ooo_-,58...6,s _ ' "!
TO WATER14_JNAGEMENTSECTION
["-- OXYGEN -- '_- --- REFERENCE 1J FROM OXYGEN CHECK- ] L_ PRESSURE FOR I
I SUPPLY _ECTiON VALVIES _WATER PRESSURE
n REGULATORS I
SU,T _'_-----_ IL I
- liFLUID FROM _IEAT EXCHANGER , WATER i
PRIMARY SEPARATORSTRANSPORT SECTION (HEATING) I
CONTROL VALVE' i
SUITSUPPLY IFLOWCONTROLVALVES SUITCIRCUIT
HEAT EXCHANGER_ (COOLING)
I FROM PRIMARYTRANSPORT
SECTION
t RETUrn tFROM
TO COCKPIT CO2 PARTIAL PRESSURIE SENSING TO VENT ._ SECONDARYDISPLAY I=qRESSOREI REGULATORS OVERBOARD - WATERWATER MANIFOLD
TELEMETRY SENSOR I RELIEF /_/ SUIT SECEVAP SHUT-OFFI VALVE STEAM _ VALVEI TO DUCTCABIN t
-0 DIVERTER IVALVEI
FANSIGNAL ICONTROL
11 ISUIT CIRCUITASSEMBLY
RETURN FAN IGAS DIFFERENTIAL
CABIN PRIES_URI[ [i RETUeN
C_CK II vALvE -- -
/ CHECK
I I \VALVES II[SELECTOR VALVE [
............._1 _*;,_....._'I-- -- '_J_J.FANS i CO2 AND O00R SUIT I
FLUID GUT_-_--_LT_._ CABIN I I REMOVAL CANISTERS CIRCUITHEAT I J
L FLUID IN _ _ .....
CABIN AIRRE_TION A'_SEMiy IATMOSPHEREREVITALIZATIONscHEMATICSECTIONI APRT30005"15766
STAGE ISOLATION VALVEWATER TO _[CONDARYTANKS I• HEATTRANSPORT
I SECTION SECONDARY HEAT
F -- -- I OR
i , CHECK VALV1[S_ [_//
_1 I _ OVERBOARDI SE.CON_ _ / _C GLYCOL _J I_..( VENT
. PR=,OREE,..FLO. I
-yWAT E R REGULATOR
,.oooLE "\\ =:_SUIT CIRCUITJ PRESSURE • 'f¢: SECONDARy HEAT
TRANSPORT SECTIONI REFERENCE / SEC SUIT FLUID./ E_PFLOW
/ \ ATMOSPHERE REVITALIZATION
/ _ESSURE CHEC DI I PRI HTSWATER / REGULATORS VALVE EVAPORATOR
SELECTORkVALVE - t
PR] WATERI EJ CHECK [4 _ DRINK
I_ _ - ----lIP PRI HTS FLUID,_*CSNT__,,_,__=__. _-._L_ ,,,.ssN,G,sDESCENT STAGE I _ -t=='arJI : FILL SEP WATER FROM
GSE _ "_ ,ARS WATER
SEPARATORSDISC GUILLOTINE
II
IDESCENT __ I WATER MANAGEMENT SECTION
T 3O005 - 156
STAGE I PLSS SCHEMATICWATER ;SE I & DRINKNOV 66
TANK HSC t STATION
ASCENT STAGEIDESCENT STAGEw
VENT
COOLANT t_ ,_t,_. _ OVERBOARD PRIMARY I ELECTRONICACCUMULATOR ...... WATER EQUIPMENT
t PORATOA VENT -- COLD PLATES
OVERBOARD
IL_ ',,
FROM PRIMARY WATER SECTION _ IL(_ ELECTRONIC
FROM SECONDARY EQUIPMENT
WATER SECTION _) ICOLD PLATES
--J
o___ ISFILTE R /,_ /_ EVAPORATOR SUIT
TEMPPRIMARY CONTROL
PUAMPS VALVEA P SENSOR
PUMP
, O ) O RUMP _._ SUIT
r_ GASPUMPBYPASS FLOW
RELIEFVALVES _TOCOCKPIT SUITREGENERATIVECOOLANT HEAT EXCHANGER
a CONTROL REGENERATIVEHEATCHECK EXCHANGER
VALVE _ |
SUIT HEATEXCHANGER(COOLING)
SUIT
CONTROLVALVE CAB,.HEAT
IHEAT TRANSPORT SECTION EKCHA.GERT30005-159
_. , , _ NOV 66
,._! _ . . _ _ ' _...... _ ,:. ,,, .:,-" _ "_,'J' .... 't,; • / .'i " " " _' '
( -
T 30005-33
ECS-SPACE SUIT INTERFACE ] _ov_6
1i In_A_'NY 'A'TE"E'L _INVERTER$
_-_ RELAY JUNCTION LEM/CSM ) _*Z]IOX UMBILICAL
UMIILICAL J DEAl)FACE REI.AY IGXCll PANEL
CENTER SIDE PANEL
R/H C|
R/H CENTER SiDE
DESCENT COMPONENTS
/_ AO,,u=,
SWITCHING CONTROL
QUADRANT _" r-t RELAY BOX ASSEMBLY
BA;;EAR Y QUADRANT 1BAT T E RY
BATTERY
I EPS COMPONENT LOCATION I DEc'r_'°°°"-"ee
T 0 ESoCuIIENTEIF ?
i,_,,,,_i i I , \, I _ I
I÷_= I I 1L j 1.- ,, ..... o .I+,v-- ', I 1_ ", "w" ' 1 , _°"_• '\
', +20V DC
• 'LI_._<_ .... i- z.,_ t_.,.....rr r.:.I/, / _.. _r...<:._, .,., ._K':j- '' '_ l .4
[ EPS FEEDER SYSTEM I ,,ooo,-,,,:':NOV 66
ELECTRICALPOWERSUBSYSTEM
lID ',_
0 _I11
> 28 VDC _ INVERTER NO.I TO
DCTOAC ACPOWER '_ LMACn.-
o LOADS=E I :.
I!
,'J,I
o 28voc .. ,NVERTER"0.2 _ ACPOWER ..I LMTOu_ "1 DC TO AC I _ AC---I I m LOADS
0> I= AC'PWR '_
INV1 --W
OFFINV2
AC DISTRIBUTIONBLOCKDIAGRAM T3ooo_-2,NOV 66
ELECTRICAL POWER SUBSYSTEM
PANEL
SE IUITI I_IW2 C1_1_.3 C_qlIAT4 UCIII_I*S, BAT6 _ •
-* /o g_**_[] o'l
SiT e ON I_ O_ O_ O;1;_tT Or_q_r._r CFm_I[Too- I1_,__ A _-_1Ir_
I CONTROLS AND DISPLAYS I T3OOOS-itsDEC 66
\
f_
_". '_ I, .,_l,_¸ _ rL ¢
" l"
t ¸' _..... \_,:::.....,,i_.-.-,- ":'"-" i
'I
1
EXPLOSIVE DEVICES- LOCATIONS I T30005-26JUNE 66
IrLECTROEXPLO$iVIr DEVICES _ _ '_ • .
PYRO pyRo BATTERYARM _eOMli_llD ' EXPLOSIVE DIEVICES ' _'_,
A I ICONTROLPANEL " ' r
-I _ PYfl_ BUS W I_MEO J_ PRESSURIZATIONRCSF_. _. _! _ .AshY. J ELeC'rR,_XeL_IVE
I_ ,_,,L'_'_ ARM DEVICI_ FIRE FIREJ .-- SWITCHING SWITCHING ENABLED COMMAN[_
LOGIC PYRO B4J6"B",_IED LOGIC _SCENT He
•/_"'L I _U,ZAT,O_'1
BATB
r i lP_L
I COt6_NGS ODCSMT SE(_JENCE STA_
'T n °'_orm I--'" [_--"I I_R LOGIC
--T-. I o ,... , |
I " ..... ENABLED I NUTS II IKX.TII
I STABILIZATION I
I ..... _J ._. C_T[R I CONT_. I| L ........ JJ
FUNCTIONAL BLOCK DIAGRAM[ -I _o,._°°s-_'.., _. . ) _ ,- ELECTROEXPLOSIVESYSTEM
I ATTITUDE ATTITUDE RATE COMMAND_
CONTROLLER
TRANSLATION I TRANSLATION COMMANDSCONTROLLER I
RANGE RENDEZVOUS RANGE RANGERATE
RANGE RATE RADAR TRACKING ANGLES TRIM COMMANDSTHROTTLE COMMANDS ?
t LM ENGINE ON-OFF CONTROLINERTIAL ATTITUD I_ GUIDANCE =" ELECTRONICS
CREW ATTITUDE MEASURING ACCELERATION COMMANDSDISPLAYS UNIT COMPUTER SECTION
RCS JET COMMANDS
ALTITUDE LANDING ALTITUDE _ '_- _
ALTITUDE RATE RADAR ALTITUDE RATE \"
t DISPLAY COMPUTER INPUT UPDATE DATA m, ABORT
l GUIDANCEALIGNMENT STAR SIGHTING DATA ...... _ 81 AND READOUT SECTIONOPTICAL KEYBOARDTELESCOPE
DEC 66I PRIMARY GUIDANCE AND NAVIGATION SECTION I T3ooo_-,_
[ATTITUDE AND VELOCITY INFORMATION CREW
-_ I '°,SPLAYSATTITUDE AND TRANSLATION COMMANDS
PRIMARYGUIDANCE
AND
l t NAVIGATION PRIMARY FLIGHT Ii CONTROL SIGNALS | MAIN
HAND IUPDATE LINK I CONTROL ENGINE CONTROL PROPUL-
CONTROLLERS ELECTRONICS COMMANDS I_SION ANDRCS
SECONDARY FLIGHT! I CONTROLSIGNALS
ABORTGUIDANCE
BACK-UP FLIGHT CONTROL SIGNALS
MANUAL ENGINE ON-OFF COMMANDS
';_"_ t * '_""' LM GUIDANCE, NAVIGATION I" ' AND CONTROL SUBSYSTEM
;.... _,T", I_T30005-44DEC 66
.r
ALTITUDE _ ; _ _ "_RATE,_,2 I ..... JALTITUDE
(VERTICALVELOCITY)
FORWARD (_.-AXIS) AND j,,_,[-)"LATERAL (Y'AXIS) VELOCITY
i --3-2 -~
/
VELOCITY ALTITUDE
TRANSMIT ANTENNAS RECEIVE ANTENNAS TRANSMIT ANTENNA RECEIVE ANTENNA
® ® ® 6) ® ® ® ®
Ft + Dt * + D3 F2+FR
_2 FR
i ..,.s...,_.l ITRANSM'TTERIt
ALTITUDE IVELOCITYCOMPUTER COMPUTER
v,-,T,C,,.,,,.oc,,Y,o,*,,,,,,,,,,.oc,,',_i .ocL"T,TU_
-L
:i L
L
..-LI s..voI.ANOAL L:WI MOTORS I CONTROL -'- _ " r
0 .a:"I ! / x
_7 / ./ _. TRACKING ANGLES •
RESOLVERS
I CARRIER DIFFERENCE DISPLAYS
SIGNALS
I DOPPLER RANGE RATETONE TRACKER -'-
MODULATION _ TRANSMITTERIMODULATION DIFFERENCESIGNALS
CARRIER REFERENCE I PHASE RANGE
TRACKER -"-
FREQ.SYNTHESIZER
I RENDEZVOUS RADAR I ,_._3°°°5-'°8_8
h,,.,L,,......
,_u.,_._ t " ,,, ' "";,r ' C.... ' " "_.
CREWDISPLAYS
Ii I
_'_ ,.
..>eJ
V?J
A /V
LAN DING R E NDEZVOUS
RADAR RADAR
ANTENNAPOSITIONCOMMANDS
IRADAR I
TEST SIGNALS _ "_" ,,,o=._.,_--
" :'_.;.=".... ,,-,- ANTENNA '
_":: _.......... POSITION• ,_:' o=,- COMMANDS.',,,w),.
TEST SIGNALS
PANEL l-n"RADAR CONTROL T3OOOS-_4
DEC 66
PRIMARY -1GUIDANCE _1 UPDATE DATANAVIGATION ISECTION _J
ABORT GYRODATA ]SENSOR ACCELERATION ATTITUDE ERROR
ASSEMBLY SIGNALS
ABORT CONTROLELECTRONICS ELECTRONICS
ASSEMBLY SECTION
ENGINE ON-OFFCOMMANDS
DATA ENTRY _ COMPUTER INPUT8 DISPLAY 8 READOUT rASSEMBLY
FEB 66[ABORTGU=DANCESECT=ONI ,_ooo_-._
• ]
it
t I ¢
J
. RCS JET COMMANDS
PRIMARY I
GUIDANCE _ THROTTLE AND TRIM COMMANDSNAVIGATION
SECTION j_ ENGINE ON-OFF COMMANDS
THRUSTCOMMANDS _
TRANSLATION DESCENT TROTTLE,TRIM,ANDENGINE ON-OFF COMMANDS DESCENTCONTROLLER . TRANSLATION COMMANDS CONTROL _ ENGINE
ASSEMBLY
ENGINEON-OFF TRIMCOMMANDS COMMANDS
RATE RATE ATTITUDEANDSIGNALS RATE SIGNALS TRANSLATION ON-OFF COMMANDS RCS
CREW= _ _ THRUSTERSDISPLAYS GYRO CONTROL
ASSEMBLY
ATTITUDE RATE AND PULSE COMMANDS
ATTITUDE _CONTROLLER HARDOVER
ATTITUDE ERROR SIGNALS
ABORT /
GUIDANCESECTION . ENGINE ON-OFF COMMANDS
I •ON-OFF COMMANDS ASCENT
MANUALENGINE ENGINE _ ENGINEON-OFF COMMANDS SEQUENCERm
I CONTROL ELECTRONICS SECTION J _..T_°°°5-'T66
+ X VEHICLE DIRECTION
13° _.1°
13" PITCH PIVOT
PUSH TO TALKNEUTRAL POSITIONOF GRIP ABOUTPITCH AXIS
r_? j YAW,x,s-PITCH PITCH
TRIMIL DECA
MODE CONT.
_ PULSEDIR
ATTITUDE I
- DEADBAND " LOGICo
RATE oCOMMANDS
FROMACA GUIDCONTPGNS
RATE NARROW _'_"SIGNAL -I DEADBAND AGS
FROMRGA
DEAD BAND ,,,/ " "MAX
ON -OFFJET COMMANDSMIN DRIVERS =' RCS
PULSE COMMANDSACA
RCS JET COMMANDSLGC
ATTITUDE AND TRANSLATION CONTROL ASSEMBLY J T30005-107APR 66
............:i'U''-_ i" ENG ARMABOR ASC
....................up.......... r!_ DES
I
CONTROt."OGJC t.MA'.
_" I L_'°_cAUTO STOP _- DES. ENG. ON-OFF j _PROPULSIONAGS< L . _)
II
GUID CONTPGNS
AGS
I ENGINE SEQUENCER I T30005-1o5APR66
MANTHROT THR CONTCOR AUTO
SE MAN
I-MANUAL THROTTLE
TRANSLATION f _.o THROTTLE CMD
CONTROLLERS
MANUAL THROTTLE T
AUTO THROTTLELGC
GUID CONT _oPGNS
o
" (T _A" i1
.,_;'_, LGC AUTO RIM. I
........... TRIM CMD DESCENTENGINE
ATCATRIM T
ENGINE ENGINE ON-OFF _ DESCENT ENGINE ENGINE ON CMDSEQUENCER CONTROL LOGIC
I DESCENT ENGINE CONTROLASSEMBLY T_O00_-,06APR 66
_ _"_'_'_16.,.A,oc.Assoc,ATEoD,SP,AYSI _.oooo-.o....
VEHICLEPOSITION
8=VELOCITYINFORMATION
POSITIONL AND
COMMANDS _I LM GUIDANCE, NAVIGATION AND CONTROL SUBSYSTEM F VELOCITYFROM -ICREW CHANGES
PRIMARY SECONDARYVEHICLE VEHICLEGUIDANCE GUIDANCE
T30005-43DEC 66
PCM DATA FOR TRANSMISSIONCOMM.
I
INDICATION TO CREW _ CAUTION AND WARNING INDICATION TO MSFN
I ELECTRONICS ASSEMBLYCREW DISPLAY DRIVE
DISPLAYS L SIGNALS
OUT- OF- TOLERANCE PULSE
SIGNALS
CODE
I I O-SVDC ANALOG DATA
VAR IOUS ANALOG _ MODULATION
SIGNALS SIGNAL CONDITIONING
w ELECTRONICS ASSEMBLY| _ AND TIMING
J DIGITAL
STATUS DATA ELECTRONICSSENSORS
ASSEMBLY
DISCRETE DIGITAL DATA
-ITIME REFERENCE SIGNALS
AUDIO AND J J TAPE RUNNING
COMM, VOX SIGNALS DATA STORAGE INDICATION _ CREW DISPLAYS
-I ELECTRONICS ASSEMBLY TIMING AND SYNC SIGNALSSUBSYSTEMS
I LM INSTRUMENTATION SUBSYSTEM I T30005-57DEC66
If- "R
DISCRETE IBUFFER
ANALOG IBUFFER
DC ATTENUATOR I
DC AMPLIFIER I
* PCMTEASENSOR ._.=,.I i C/WEA,OUTPUT > "_="< __ 8 DISPLAYS
R/DC CONVERTER
AC/DC CONVERTER IVARIOUS ANALOG SCALED (0-5 VDC) ANALOG
AND DISCRETE AND DISCRETE DIGITALSIGNALS SIGNALS
FREQ/ I IDC CONVERTER
I PHASE IDEMODULATOR
L --J
I SIGNAL CONDITIONINGELECTRONICSASSEMBLY I "r3ooo5-_,MAR 66
[
--,NO_lw.--oI sE.'_ LW--O,NO,C.T,ONWARNING v (ONE OF TWENTY)
v DETECTOR RESETI LOGIC
SIGNAL I CHANNEL i-- I
•Ill i i illI III ir IllOUT- OF-TOLE RANCE
SIONALS I _1 In IJJ
I
DETECTOR RESETI CAUTION v lONEOFTWENTY)
s,o_,,-I CH_NEL I -' LOGOCL.. ..... J
PUSH-TO-RESET RESET I MASTER I_SET
v ALARM 1_I .oo,cMASTER INDICATION
I | L_IIPSYSTEM ENGINEERS HEADSET(ONE OF TWO)
ICAUTIONAND WARNING ELECTRONICS ASSEMBLYT 50005- 48DEC 66
MASTER ALARM SIGNAL (DIGITAL)C/WEA
SENSORS .'-:-D" I DIGITAL DATAAND
SCEA
I _\_L' .._}P_.LL_LANALOG DIGITAL I DIGITAL I
I TO I • DATA =I DIGITAL DATA j OUTPUT SERIALDIGITALDATA COMM.MULTI- -
DIGITAL _ ..._ PLEXER I REGISTERSERIAL /CONVERTERI---_JPAM
DATA
CONTROL CONTROLCOMMANDS COMMANDS
-"'_1 HIANALOG RATE
NLOGISCE i MULTI- _ SELECT
PLEXER _ CONTROL COMMANDS LO
PARALLEL
DIGITAL
TIMING
DATA TIMINGSYNC,
"I__"
SERIAL DIGITALTIMING DATA ] TIME _ TIME REFERENCE TIMING
DSEA_-_ ACCUMULATOR GENERATOR
TIMING SYNC ]SUBSYSTEMS
PULSE CODE MODULATIONAND TIMING ELECTRONICS ASSEMBLY T_os-sBAPR 66
r
COMM J VOX TRIGGER S!ONAL
L I " lvoDc£ _ VOICE TAPE
] i 'AMPLIFIER DRIVE _ (N_ILE sl_Ju.
MOTOR
RECORDER •( TAPE ON
:" "5 D @DIGITAL I ..... "
TIMING TIME I UI_,_T.JU-_m i I '----''_lASSEMBLy : AND DRIVE
TRIGGER SIGNAL
SYNCHRONIZATIONSIGNAL
IDATASTORAGE ELECTRONICS ASSEMBLYJ MAR.T30005"4"
I INSTRUMENTATIONASSOCIATEDDISPLAYSJ _sooo6-,,,,APR 66
OUT- OF-TOLERANCE SUBSYSTEM STATUSINDICATION INDICATIONTOCREW TO EARTH
SUBSYSTEM _ AUDIOSTATUS FROM
SENSORS / COMMUNICATIONS
SYNC. RECORDINGAND OF
TIMING AUDIO
T50005-42MAR 66
DATA VOICE
R_GING
_ _.i.....i, - ...................
INFLIGHT COMMUNICATIONS CAPABILITY-_EARTH SIDE "r3ooos-38FEB 66
II-
II
II
II
I
¢//
//
//
!
I INFLtGHT COMMUNICATIONS CAPABILITY_FAR SIDE __iT30005 -39JULY 66
EARTH
COMMANDMODULE MOON
OF SILENCE
NOT DRAWN TO SCALE
I COMMUNICATIONS DURING LUNAR STAY] T3OOOS-,OIMAR6e
I 1VHF S-BAND S-BAND I S-BAND IINFLIGHT EVA OMNI ERECTABLE STEERABLE
ANTENNA ANTENNA ANTENNA ANTENNA I ANTENNA I
vT_Y,'..-.-.T'.,,5 °-<I S-BAND I
DIPLEXER I
I -T I I
VHF DIPLEXER I I AMPLIFIER I
, L f___ _I I .
__ VHF/AM I
TRANSMITTERS/ I I S-BAND Ii(2) I
RECEIVERS I ii.Ra_ t TRANSCEIVERS
(2) _ T-- ----
Lr "£R;-, - I ,
' I auD'° L J _EMODULATIONI ' I II CENTERS(Z) F -IPROCESSOR(PMP)IJ TV CaMERa
, I , T -I _, ''! PC. II J ,I TELEMETRYI -I osEa I'-- I
L__ _ __ _ I I
II SUBSYSTEM/ I I IISENSORS I SUBSYSTEM J)JL (IN INSTRUMENTATION
I LM COMMUNICATIONS SUBSYSTEM I oect3°°°s-3t66
÷X
VHFANENNA(2)
ASCENTSTAGES-BAND STEERABLEANIT..NNA DOCKING EVA
HATCH
RENDEZVOUS DOCKING TARGETRADAR
AN11_INA AFTEQUIPMENT BAY
OVERHEADDOCKING
S-BAND RCSPITCH INFLIGHT THRUSER
ANTENNA(2) ASSEMBLY
INGRESS/ RCSNOZZLEEGRESSHATCH
LANDINGGEAR
+Z ROLL
DESCENTEGRESSPLAITORM DESCENTENGINE
SKIRT STAGE
ILUNAR MODULE T30005161AXES NOV66
COMMANDER'S
AUDIOPANEL 1
FROM MIC l AUDIO VHF
i C SECTION
_= TO HEADSET I% ER VOICE
COMMANDER EKG 7"I
SIGNAL vOiCE, EMU, S BANDEMERG KEY PROCESSOR BiOMED, PCM, SECTION
ASSEMBLY EMERGKEY .ERA-4
SYSTEM / EKGENGINEER L TO HEADSET PCM, TIMING
I FROM MIC . PREMODULATION I INSTS
I PROCESSOR voice
SYS.ENG. lAUDIO ANDCOMM.PANEL
SIGNAL PROCESSOR ASSEMBLYIINTERFACE T30005-53DEC 66
| '1I CHANNEL"A" II I
- , _7_7' I
S-BAND VOICE VHF RCVR I
1 l l,"/SIGNAL L IRCVD VHF VOICE,EMU _ PROCESSOR DIPLEXER - -
(TO s BAND XMTR) _ / ASSEMBLY
J II B-CHANNEL
VOICEFROM VOICEI J
"l W XM,,iI :VOICE,EMU I VHF RCVR I
l II ERA-5L
VOICE TO CREW
I I(VOICE TAPERECORDER)
(IN INST. SUB- SYSTEM)
PCM(LO BIT RATE)
I VHF-SECTION I rsooos-5_DEC 66
r _'l
' LIVOICE I RECEIVER
SUBCA'RRIER4 I PRN (PRIMARY O_ r|
i _ SECONDARY)
I /
F-
kBA(C_-EUP_ MODULATOR MLILTPLIER AMPLIFIERPMENABLE (PRIMARY OR (PRIMARY OR (PRIMARY OR DIPLEXER
i-_ SECONDARY) SECONDARY) SECONDARY)voicE,PCM I 1
(PRIMARY ORSECONDARY)
FM ENABIF" _ _ FREQUENCY ERA-I ERA-2
MODULATOR r --"J
v,o,o..,i.v I J ,N-.uo.,_'q:z,.-_,o..','__/STEERABLE'_ II ECTABLE_ANT. NO. 11' I ANT NO 2 [_ ANTENNA !
CAMERA ' I\ ANTENNA /
' ,L0N,.STAY, __ o _, L_]. ERA-5I
STAY
S-BAND SECTION T3ooo5-56DEC 66
n_PI
imU
gl
unpi
i,ll
1_I
_lm
fl_t C
l)l I
_P-,
IIv o o
oo_
r3j
!
_B
EXTRA-MSFN VEHICULAR CSM
ASTRONAUT
AUDIO .ON-BOARD COMMUNICATIONS SUBSYSTEM TO BE
CREW RECORDED
TELEMETRY T.V.DATA SIGNAL
T50005-41DEC 66
SUBSYSTEMS MSFN,CSM,EVA ELECTRICALEQUIPMENT
STATUS , DATA,TV I THERMAL
MANAGEMENT
INSTRUMENTATION TELEMETRY :1[ COMMUNICATIONS Vlo-VJ_--DEO_>CAMERA ENVIRONMENTALcoNTROL
I VOICE
STATUS INFORMATION _1 I- LIFE SUPPORT
-I F_CREW CONTROLS,
FIRE COMMANDS AND DISPLAYS DATA ENTRY AND DISPLAY
½ F 1GUIDANCE
EXPLOSIVE NAVIGATIONPOWER ENGINE AND CONTROLDEVICES CONTROL CONTROL
<_ AC I ELECTRICAL PROPULSION I- ENGINEcoNTR°L
SUBSYSTEMS _ DC I POWER AND RCS F
I LM SUBSYSTEMS T3OOO5-6oDEC 66
