Apollo 11 Final Flight Plan Revision A 555h15
This document was ed by and they confirmed that they have the permission to share it. If you are author or own the copyright of this book, please report to us by using this report form. Report 3i3n4
Overview 26281t
& View Apollo 11 Final Flight Plan Revision A as PDF for free.
More details 6y5l6z
- Words: 5,691
- Pages:
Memorandum Distribution
TO
:
FROM
: CF/Chief,
SUBJECT:
Revision
DATE:
Flight
Crew
A to the Apollo
Flight
8, 1969
In reply refer CF3&2-9M-133
Division
11 Final
July
to:
Plan
Enclosed is Revision A to the Apollo 11 Final Flight Plan. Enclosure 1 contains the pen and ink changes to be made on the indicated pages. Enclosure 2 contains the new pages which replace the same numbered pages in the final edition of the flight plan. Changes on the new pages are made with prestige elite type rather than gothic type so they will be readily evident.
Enclosures
2
CF342:TAGuillory:jat
7-E-69
Buy U.S. Savings Bonds Regularly on the Payroll Savings Plan
ENCLOSURE 1 MAKE THE FOLLOWING PEN AND INK CHANGES TO THE FINAL FLIGHT PLAN CHANGE
PAGE 1-7
ON "LM POWEREDDESCENT/HIGH GATE TO TD" FIGURE CHANGE ORDINATE AND ABSCISSA FROM "FT" TO "FT X 103"
l-10
ON TABLE l-3
FIRST COLUMN CHANGE "1409
ON TABLE l-4
CHANGE Al LONGITUDE FROM 60.500"E
-
1-11
CHANGE Gl DELTA ALTITUDE FROM -001.97
1-17
PARAGRAPH Ei, CHANGE TIMES: 103:30:00-TO 107:15 148:00:00 TO 151:00 154:00:00 TO 172:00
2-31
& 2-32
2-44
CHANGE TITLES
EDT" TO "1209
EDT"
TO 65.50Q"E
TO -001.76
FROM "PHASING" TO "ASCENT PHASING"
CHANGE 275 (+0418.1)
TO 275 (tO418.5)
CHANGE AVX, AVY, AND AVZ BLOCKS FROM 00 0 - -*TO 00 ----2-48
CHANGE AVR N42 BLOCKS FROM + 0 CHANGE F/A, TO 00 ----
R/L,
0
AND D/U BLOCKS FROM 00
CHANGE "S-IVB
TO ORBIT CAPABILITY"
TO + 0 ----0 ---
3-ii
AT 05:25
TO "CO1 CAPABILITY"
3-l
AT 00:37 CHANGE "ECS REDUNDANT COMPONENTCHECK" TO "SEC GLYCOL LOOP CK" AT 00:43 IN BOTH COLUMNS CHANGE "RECORD AAZ CORRECTION" TO "RECORD Z TORQUE"
3-5
AT 04:07
DELETE "THRUST MONITOR - P47"
AT 04:52
DELETE "MANEUVER TO OBSERVE SLINGSHOT"
3-6
AT 05:lO
IN MCC-H COLUMN "ADD
3-10
AT 11:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "MCCl WILL BE DELAYED TO MCC2 IF PROPELLANT COST IS NOT PROHIBITIVE"
3-19
AT 26:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "TO AVOID EXECUTION OF MCC3, A NON FREE MCC2 WILL BE EXECUTED (SPS BURN IF THE BT >3 SEC)"
1
------
.-__
--~
UPLINK CMC 1 ZERO TRUNNION BIAS”
CHANGE
PAGE 3-33
AT 53:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "MCC3 WILL BE DELAYED TO MCC4 IF PROPELLANT COST IS NOT PROHIBITIVE"
3-43
AT 70:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: BE EXECUTED WITH THE SPS IF THE BT >3 SEC"
3-44
AT 71:25 DELETE "PRE-LO1 ECS REDUNDANT COMPONENTCK ACTIVATE PRIMARY EVAPORATOR" AND ADD "SECONDARY RADIATOR LEAK CHECK"
3-51
AT 80:12
CHANGE "DO NOT TRIM" TO "TRIM X AXIS TO 1 FPS"
3-53
AT 82:13
CHANGE R 0,
3-54
AT 83:20
CHANGE R 82, -350/229,
3-61
AT 95:00
ADD "ROLL RT 40",
3-63
AT 96:48
IN MCC-H COLUMN DELETE "BLOCK DATA"
3-73
& 3-74
P -257/297,
Y 0 TO R 0,
P 296/303,
Y 0
Y 0 TO R 82,
P 296/229,
Y 0
TO R 122,
P 229,
Y 0"
DELETE LOCAL HORIZONTAL PITCH OF 166.3 107:14 RESPECTIVELY
& 244.2
3-76
AT 109:45
IN LM COLUMNS ADD "RADIATION
READOUT"
3-79
AT 112:30
IN CMP COLUMN ADD "ACTIVATE
3-83
AT 116~40
IN LM COLUMN ADD "CONFIGURE COMM (TV-OFF)"
3-91
AT 126:00
IN MCC-H COLUMN ADD "DUMP DSE"
3-92
AT 126:07
IN LMP COLUMN CHANGE P -58 TO P +58
AT 106:47
AND
PRIM EVAPORATOR"
AT 126:30 CHANGE CSM ATTITUDE FROM R 180, TO R 0, P 239/160, Y 0 3-93
"MCC4 WILL
P _264/177,
Y 0
AT 128:00 ADD IN CMP COLUMN "EXT RNDZ LT - OFF" AND IN MCC-H COLUMN "DUMP DSE" AT 127:00
IN CMP & MCC-H COLUMNS ADD "GO/NO GO FOR PYRO ARM"
3-95
AT 130:00
IN MCC-H COLUMN ADD "DUMP DSE"
3-100
AT 134:12
DELETE "ECS REDUNDANT COMPONENTSCK"
3-101
AT 135:18 R2=lllll"
CHANGE "DAP - Rl=lOlll AND MOVE TO 135:05
3-102
AT 136:15
ADD "DEACTIVATE PRIM EVAPORATOR"
3-132
AT 192:27
CHANGE "MENKAR (07)
2
R2=11111"
TO "DAP - Rl=lOlOl
ENH" TO "MENKAR (07)
EFH"
ENCLOSURE 2 SYMBOL NOMENCLATURE
ff
l--
LUNAR PENUMBRA (OCCURS PRE LOI,)
PENUMBRA(PRE EI)
ALSO EARTH
SPACECRAFT SUNSET
.
M S F r?
b 4---
MADRID 85FT DISH COVERAGE DARKNESS (UMBRA) MSFN LOS
I:--!
.
SPACECRAFT SUNRISE LUNAR PENUMBRA (OCCURS PRE LOI,)
ALSO EARTH
PENUMBRA(PRE EI)
-3 c---LUNAR
IMSFN
SURFACE
AOS
HONEYSUCKLE85~~ DISH COVERAGE j_cGOLDSTONE
85FT DISH COVERAGE
LUNAR TERMINATOR SPACECRAFT SUNSET
DARKNESS
+-LUNAR
TERMINATOR
xi
Revision
A
INTRODUCTION This Flight Plan has been prepared by the Flight Planning Branch, Crew Division, with technical by TRW Systems. This document schedules the AS-506/CSM-107/LM-5 to fulfill, when possible, the test objectives quirements, G Type Mission Lunar Landing.
operations defined in
The trajectory parameters used in this Flight Plan launch, with a 72" launch azimuth and were supplied Analysis Division as defined by the Apollo Mission Trajectory.
Flight
and crew activities the Mission Re-
are for July 16, 1969 by Mission Planning and G Spacecraft Operational
The Apollo 11 Flight Plan is under the configuration control of the Crew Procedures Control Board (CB). All proposed changes to this document to the CB via that fall in the following categories should be submitted a Crew Procedures Change Request: 1.
Items
that
impose
additional
2.
Items
that
impact
the
3.
Items
that
result
in a significant
4.
Items that day in the
result Flight
in moving Plan.
5.
Items that
require
The Chief, Flight fall in the above
training
accomplishment
a change
Planning Branch categories.
Mr. T. A. Guillory will act the Apollo 11 Flight Plan.
crew
major
or impact
of detailed
test
RCS or EPS budget activities
to the
flight
as co-ordinator
change.
all
activity
file.
determine for
what
proposed
proposed changes
Any requests for additional copies or changes to the distributicn this document must be made in writing to Mr. W. J. North, Chief, Division, MSC, Houston, Texas.
xii
procedures.
objectives.
to a different
data
(FCSD) will
crew
lists Flight
changes to of Crew
b.
The coolant loop operation will be as follows: Launch - primary loop operation (1) Earth Orbit - primary loop operation and secondary (2) loop test Post TLI - deactivate both evaporators (3) Pre LO1 set rad leak ck only. (4) At 112:30 activate primary evaporator (5) Post TEI - deactivate primary evaporator (6) Entry interface minus 1 hour - activate primary and (7) secondary evaporator.
3.
Guidance and Navigation a. During lunar orbit, the CSM and LM will utilize the same landing site REFSMMAT such that the gimbal angles would be O,O,O at landing with the LM sitting face forward on landing site number two and the CSM over the landing site pitched up 90" from local horizontal "heads up". b. During PTC the CSM/LM x-axis is Ditched up 90" (North)%A for TLC and down 90" (South) for TEC with the Y-Z axes This change in x-axis in the plane of the ecliptic. pointing is to enable simultaneous viewing of the earth and moon through the side windows while maintaining a favorable hiqh aain antenna oosition. c. The CSM tracking light will be on continuously from undocking to landing and from LM lift-off to docking.
4.
Landmark Tracking The following ground rules were used for landmark tracking. a. IMU to be realigned on the dark side preceding each tracking period. b. MSFN is reacquired after each tracking period. The tracking data will be acquired by MSFN after all the marks have been made and while N49 (hR,hV) is displayed. MSFN will give a GO when data acquisition has been verified. c. The pseudo landmark tracking (Al) will be used to determine the altitude of an area in which the LM will be making altitude checks after DOI. The data will be processed during the sleep period after the trackings and relayed to the LM prior to undocking.
1-18
Revision
A
d.
e.
f.
F.
In the docked configuration the CSM/LM approaches the landmark in an inertial hold attitude. This inertial attitude + places the spacecraft 2" below the local horizontal at the 35" elevation angle point. At 35" elevation angle a pitch down of 0.3"/sec is initiated. Five marks are then taken with the time between marks a minimum of 25 (See tracking profile) seconds. In the undecked configuration the CSM approaches the landmark in ORB RATE and. pitched down 22" from the local horizon- ' tal. At 35" elevation angle five marks are taken with the time between marks a minimum of 25 seconds. ORB RATE is continued throughout the marking period. In the undecked COAS tracking the CSM will approach the LM in ORB RATE heads up and pitched down 40" from the local horizontal. When the LM is centered in the COAS the CSM will initiate a variable pitch rate to keep the LM centered in the COAS.
MZO
v
es
\\,i
HY+k
,' \
9
,;c
q\ -------Q &<
I
5.
CSM/LM and CSM attitude maneuvers will normally be at a rate of 0.2"/sec or 0.5"/sec. unless other rates are required. NOTE: At 0.2"/sec,15 minutes is required to maneuver 180". At O.S"/sec, 6 minutes is required to maneuver 180".
6.
ive thermal control mode will be initiated after MCCl or as soon as MCCl is scrubbed and maintained throughout the mission (except in lunar orbit) until at least three hours before entry except for interruptions for midcourse corrections, communications orientation (maximum interruption of three hours). PTC will not be initiated before approximately 7:00 GET.
7.
Service Propulsion System All SPS burns will on Bank A except LO11 which will be initiated
be initiated on Bank B.
LM Notes 1. Entries into the LM a. Three entries into the LM are scheduled in the at 56:30, 81:30 and 95:52 GET respectively.
1-19
timeline
FLIGHT PLAN 1730 EDT
CMP
LMP
CDR
CLEAR TUNNEL OF CM HATCH INSPECT TUNNEL & DOCKING LATCHES REMOVE PROBE & DROGUE
_-.. -
TEMPORARILY STOW PROBE AND DROGUE
:lO
TRANS TO LM PWR
CSM PWRTO LM - ON (AT LMI' REQUEST)
-
ACT VHF B FOR DATA XMIT FOR 5 IMINUTES
:20
-TRANS TO CSM PWR
DUMP DSE (LM DATA) IVT TO LM
PWRTO LM - OFF (AT LMP KEQUOST)
-
OPERATION OF LM 16mm CAMERA
:40 LM FAMILI
-
L
’ MISSION APOLLO 11 f:;T)
(:Tr.,, :
l&vision
(IZATION
LM FAMIL
lIZATION
:50
57:oo
DATE
EDITION j
ASSIST CDR
L 56:30
PTC
I;~?,T; 21"'
.~~
OPEN LM HATCH RECORD ROLL CAL ANGLE IVT TO LM
CONFIGURE DSE TO RECORD LM DATA
":;I:
MCC-H
LM
CSM
A
July
8, 1969
-__ FLIGHT PLANNING
TIME 56:00
- 57:00
BRANCH
DAY/REV 3/TLC
PAGE 3-35
-
T
LOI, BURN CHART
LOI,
P OR Y RATES
ATT DEVIATION
loo/SEC TAKEOVER
+lO" TAKEOVER
SHUTDOWN
PESIDUALS
TIME BT + 10 SEC
DO NOT TRIM
LOI, ABORT MODES
2924.0
TRAJECTORY
'GO
BT
- 2129.0
O-01:50
Lo1l
2129.0
- 1589.0
1589.0
- 0
01:50 03:oo
03:;;
is
HYPERBOLIC
ABORT MODE MODE MODE II
(UNSTABLE
LUNAR ORBIT
MODE III
3-46a
I - COAST 2 HR - OPS - P37 (P37 BEYOND SPHERE FOR VGO >2279 AND BT <01:3( - COAST 2 HR - 2 DPS BURNS FOR STABILIZATION AND bfATEt? or CLA LANDING - DPS BURN AFTER ONE REV
Revision
A
2130 EDT
MCC-I4
_ -
84;O0 84:Ol
FLIGHT PLAN
NOTES
l-
j 02 FUEL CELL PURGE
5M PRESiEEP CHECKLIST CREW STATUS REPORT ,\, (RADIATION & MEOICATION) ,YCLE 02 & H2 FANS IHLORINATE POTABLE WATER SELECT NORMAL LUNAR COMM CONFIGURATION - EXCEPT: S-BAND SQUELCH-ENABLE HGA TRACK-REACO HGA BEAM - NARROW IIERIFY: WASTE MNGMT OVBD DRAIN-OFF WASTE STOW VENT-CLOSED EMERGENCY CABIN PRESS-BOTH SURGE TANK 02 VALVE-ON REPRESS PACK 02 VALVE - OFF POTABLE WATER HTR-OFF iL LM TUNNEL VENT VALVE-LM PRESS
1 REV 5
;
84:30
-
84:33
EAT PERIOD
'02
FILTER CHANGE NO. 7
9 INTO A, STORE 7 IN B6
MISSION
1
EDITION
APOLLO 11 YSC Form 29 (yay
FINAL 69)
DATE
I
JULY 1, 1969 fLlOn1
RINNINO
TIME 84:00
BUANCH
- U5:OO
DAY/REV 4/5
1 PAGE 3-55
LUNAR ORBIT REST PERIOD ATTITUDE
LOCAL HORIZONTAL
I LOS EARTH 3-55a
Revision
A
FLIGHT PLAN MCC-H
LM
CSM 1130 EDT
CMP
LMP
CDR
98:00
MANEUVER TO TRACKING ATTITUDE R 0 ,P297/27O,YD DOFF HELMET & GLOVES 98:21 SELECT OMNI C
DON HELMET & GLOVES
DON HELMET & GLOVES
ARS/PGA PRESSURE INTEGRITY CHECK
ARS/PGA PRESSURE INTEGRITY CHECK
CABIN REGULATOR CHECK
CABIN REGULATOR CHECK
DOFF HELMET & GLOVES
DOFF HELMET & GLOVES
COPY DAP DATA COPY GYRO TORQUE ANGLES AND FINE ALIGN IMU
SELECT OMNI -FWD BIO MED SWITCH - RIGHT
X
98:30
) z
, Y
GO INERTIAL UNSTOW OPTICS P22 ORBITAL NAVIGATION
UPDATE LM DAP DATA GYRO TORQUE ANGLES
OPT:ICS LMK ID 130 T1 9 8: 4 0: 0 2 (HOR) T2 1yr.4 5.08(35") 4.6 NM @i%g'--mRATE GYRO CHECK
4GS ACT & SELF TEST
N 89 LAT +ocl.2 4 LONG/Z + 11..8 4 ALTITUDE- ,o 0 l..A&NM
RO,P126.5/22.5,YO CONTINUEPITCH TO AGS CAL PITCH ATT (22.5)V64 ACQUIRE IdSFN ANT P 187, Y 70
V64 ACQUIRE MSFN
MISSION )Gp','; j:r,lrr,
1
EDITION
Revision APOLLO 11 'IF,, (c)T) (:j<-: I:)
DATE
I A
July
8, J9hY FLIGHT
TIME
I 98:00 PLANNING
- 99:00
BRANCH
DAY/REV 5112
DUMP DSE
PAGE 3-65
I
3 4
1
FLIGHT PLAN CSM
LM 1230 EDT 99:oo
CMP STOW FLIGHT PLAN UNSTOW SOLO BOOK COPY PADS
MCC-H
CDR
LMP
UPLINK LGC
DRIFT CHECK-REPORT GIMBAL .ANGLES & TIME TO MSFN DEPLOY LANDING GEAR
I VECTORS LGC/CMC CLOCK SYNC PIPA BIAS LGC ABORT CONSTANT
ORDEAL INITIALIZATION LOAD DAP DATA - 32012 CSM WT -P TRIM Y TRIM DPS GIMBAL DRIVE AND THROTTLE TEST
DON HELMET & GLOVES SC CONT - SCS MIN/MAX DB, LOW/HIGH RATE (AT REQUEST OF CDR) GO/NO-GO FOR UNDOCKING DISABLE ROLL JETS FOR RCS HOT FIRE
V47 INITIALIZE
AGS
COPY AGS ABORT CONSTANT AND K FACTOR
RCS PRESSURIZATION
RCS PRESSURIZATION
m
/f%%%&r UPDATE CSM
GO/NO-GO FOR UNDOCKING RCS CHECKOUT
RCS CHECKOUT
TUNNEL VENT VALVE - OFF RECORD LM PCM DATA
SC CONT - CMC AUTO MANEUVERTO ACS CALIBRATION ATTITUDE
SC CONT - SCS RATES
MISSION APOLLO 11
1‘, . 1.I-.,.,,, 11s;I) i ( T ) (. T,..;
:99:49 - REV 13 r
1
EDITION Revision A \
DPS PRESS &; CHECKOUT
DATE July b,
TIME lYh9
F'LIGHT
99:oo PLANNING
- loo:oo
BRANCH
DAY/REV
PAGE
5/12-13
3-66
FLIGHT PLAN 1330 EDT -100:00
CMP RR TRANSPONDER ACT & SELF TEST CONFIGURE DAP GDC ALIGN TO FOR UNDOCKING, CSN ONLY Rl = 11102 R2 = 11111 SC CONT - SCS START 16HM CAMERA -mOCKI
I
MCC-H
LM
CSM
LMP
CDR DAP DATA LOAD
V47 AGS ALIGN
21112
CSM: R 0,
II DON HELMETS AND GLOVES PREPARE FOR UNDOCKING
ENABLE 83 & C4 RCS JETS V64 ACQUIRE MSFN LM INPECTION, CAMERA OFF
'AW LEFT 60", )ET ORDEAL 'AW 360".
P15 /14, /'<'
RO, P194, Y60 JPLrNK LGC
PITCH UP 110" ACOUIRE MSFN ANT P 123, Y -37
LM INSPECTION
DOFF HELMET & GLOVES COPY PADS CONFIG FOR
DESCENT TARGET LOAD PIPA BIAS
SC CONT - CMC CSM VOICE P30 EXT A’/ P41 RCS THRUSTRELAY
?
SEPARATION
c
100:48
P20 AUTO MANEUVER SXT & VHF RANGING
JPDATE LM DO1 MNVR PAD PDI PAD i PDI ABORT
lO MIN
;;o;;;gEsT
JPLINK LGC CSM STATE VECTOR (5)
LM E:
JPDATE LM piGp&m
100:54 VHF RANGING RR - OFF COPY PA0
i
.q,.,.
,.
.!
APOLLO 11 I I. \, i ,
DATE
EDITION
MISSION
Kevisior.
j
UPDATE CSM IrtUE
101:oo
A
July
TIME
8, 1969 FLIGHT
100:00 PLANNING
- 101:oo
BRANCH
DAY /REV 5113
PAGE 3-67
PAD
FLIGHT PLAN MCC-H
LM
CSM 1430 EDT 101:oo
CMP P52 IMU REALIGN OPTION 3 REFSMMAT REPORT:
LMP
CDR
REPORT: P52 (LDG SITE REFSMMAT) N71: _
--)
-.. -~
LM STATE VECTOR
N05: -_-.-N93 :
I M S
X Y _
k
z
UPLINK CMC
SYSTEMS CHECKS
_.-
--
-
_.--
-
-
_ _'--GET -----
DUMP DSE
V47 AGS ALIGN
--
GO/NO GO FOR DO1
P40 DPS THRUST MNVR TO DO1 ATTITUDE
UPDATE LM STEERABLE ANTENNA ANGLES (GET: To2:19)
OMNI AFT, PCM LBR VHF A-VOICE, B-DATA GDC ALIGN TO IMU VHF 6 - DATA P20 AUTO MANEUVER TO SEXTANT TRACK LM
1:
CONFIRM DOI-VHF RANGING INCORPORATE P76 P20 AUTO MANEUVER TO SEXTANT TRACK LM SEXTANT TRACK ONLY
101:30
SLEW STEERABLE ANTENNA CSM: RO, P215/319,YO ANT P 220, Y 28 -
- 101:41
DPS,DO ULLAGE: 2 JET, BT: 28.5 SEC
TRIM Vx RESIDUALS PITCH DOWN, P=195, RR-01 P20 MAN LOCK - ON
- 101347
- REV 14
ORUIT 8.97 RR-OFF i'%J tXl
SEXTANT'AND VHF TRACKING OF LM 102:oo
IMISSION APOLLO 11 by ,,,- ,.:,,
1' / ,.>T!
1
EDITION Revisiun A
i 1~\. 8' '
TIME 101:oo
1969
FLIGHT
PLANNING
SEC
X 57.87
LM FDAI: VHF A-VOICE/RNG __~.~~ . VHF B - XMTR - OFF SET CAMERA 16mm/HCEX(4,500,INF) 6 fps COAS OVERHEAD
AV
LOAD PDI + 12 ABORT PITCH DOWNTO 106.5' YAW LEFT 180"
DATE July 8,
7.5
- 102:oo
BRANCH
DAY /REV 5/13-14
RO, P294.9, <
PAGE 3-68
Yo
FLIGHT PLAN CSM CDR
CMP 7-
LMP
P52 PITCH ALIGNMENT CHECK
SEXTANT AND VHF TRACKING OF LM
RR - ON P20 MODE II
V06N20, ENTER ON MARK RECORD PITCH CDU N22, REOCRD PITCH CDU BATTERIES 5 & 6 ON
LOCK - ON
SYSTEMS CHECK DPS, OPS, RCS, EPS, CWEA
TERMINATE P20 TRACK
P20 AUTO MANEUVER TO SEXTANT TRACK LM
LR - ON
POO, PITCH DOWN0.2O/SEC
ij
M S
M S
LPD ALT CE YAW RIGHT 174'
N'
N'
102:53 a
i
103:oo
:nlTlnN
Kevision
(;:c$ r \
kI
PERFORM LUNAR CHECKLIST STAY/NO STAY
DATE
I
A
SYiTEMS MONITOR
STAY/NO STAY 1 STOP 16mm CAMERA INITIATE DPS VENTING 1 ASCENT ATTE ES OFF V76 RCS MIN IMPULSE REPORT !47, !;3
I
LYIIIVI.
7.5 SEC LM ;DAI:RlBO,P286.5,YO SEC 1
PO YO
0
R 0, P -206/80, Y 0 RR TRANSPONDER - OFF V64 ACQ MSFN VHF RANGTNC m . ” , . __ _ - _ _ OFF
102:35:13
"LLAGE: 2 JET, ;; =,1;7;;NF;;
THEN 6"
,';"I:
July
TIME
8, 1969 FLIGHT
102:oo PLANNING
u
START 16mm CAMERA 3ETI:
LM CONFIRM STAY/NO STAY V44 SET LS FLAG ~&I ;M&At;/NO STAY
COPY BURN REPORT GO/NO GO
N20 AGS ALIGN CONFIGURE AGS
EVALUATE MANUAL CONTROL PITCH OVER AT P64 MANUAL ATTITUDE CONTROL TOUCHDOWN
102:46
D!JMPDSE
CSM; RO, FE+77
LPD ALTITUDE, ATTITUDE POSITION CHECK, ULLAGE 7.5 SEC
1
102:30
APOLLO 11
ANT P 220, Y 28 ACQUIRE MSFN DO1 POST BURN REPORT
LPD ALTITUDE, ATTITUDE POSITION CHECK GO/NO GO FOR PDI
102:19
:.;:;“ ,li,)‘rn ~.lAC (W)
MCC-H
LM
- 103:oo
BRANCH
1 DAY/REV 5114
STAY/NO STAY STAY/NO STAY ENABLE MSFN RELAY
PAGE 3-69
FLIGHT PLAN MCC-Ii
LM
CSM 1630 EDT
CMP
LMP
CDR
AGS LUNAR SURFACE GYRO CALIBRATION LOAD AGS ASCENT TARGET ~=6O,uuO FT, H DOT=32 Fp: CLOSE SHADES, DOFF HELMET AND GLOVES
DOFF HELMET NO5: __--.-.-N93: X
_-.-.---
Y
-
-.--
AND GLOVES
-
i M j : I N
-
2
--*--ET: ALIGN GDC. ORDEE
~57-1~~ ALIGN (REFSMMAT) 2 CELESTIAL BODIES N04: __-.-N05: __-'--
8omm/BW/CHECKLIST 60mm/HCEX/CHECKLIST
p22 AUTO MNVR TO TRACKING ATTITUDE ORB RATE(IF TIME PERMIT
N71: --)-N93 : X --.---Y 2 __.--NE9 : LAT --.--LONG/2 ALT
6 FRAMES FAR FIELD (FOCUS 50') 6 FRAMES NEAR FIELD (FOCUS 20') WITH EACH CAMERA REMOVE MAGS AND STOW INSTALL PROTECTIVE COVER AND STOW CAMERAS
- 103:39
IF NOT AT 104:lO) YO
1103:45
-REV
15
t PHOTOGRAPH'LUNAR SURFACE
GET ------INITIALIZE
1
APOLLO 11 ~I,,
;‘c,.n
1'I
"Tj
f,:r,
EDITION Revision A ,
DATE
I July
8, 1969 FLIGHT
UPLINK LGC AGS
ASCENT PAD DATA
COARSEALIGN RR CDU
TIME 103:oo
PLANNING
cAozpI~U%s
INSTALL WINDOWSHADES
I
- 104:oo
BRANCH
UPDATE CSM /
COPY P57 DATA
Lt%‘Y ANIJ LlJ&J
1 MISSION
:OPY LANDED .OCATION, GRAVITY rlEASURE
AGS LUNAR ALIGNMENT
COPY LM TRACKING PAD (SEE GET - 104:35)
RO P338/76,
~57-1~~ ALIGN (REFSMMAT) GRAVITY MEASUREMENT N04: ------
RR TO STANDBY. REPORTESTIMATE OF LANDED LOCATION CLOSE SHADES
COPY AGS AZIMUTH
DAY /REV 5114-15
& VECTOR I (TD + 1:40) UPDATE LM ( ASCENT PAD
PAGE 3-70
FLIGHT PLAN MCC-H
LM
CSM CMP S/C CONT - SCS
F
1730 EDT 104:oo
CDR
P57 - GRAVITY AND ONE CELESTIAL BODY (T-ALIGN) N04: _--.-N71: -N93: X -_.--Y --.---
/ fa
P22 AUTO MANEUVER TO TRACKING ATTITUDE? ORB RATE
LMP
REPORT:
RO, P338/342,YO
2
~ GET
-
--
-.-
---I_---
DON HELMET& GLOVES CONFIRM STAY/NO STAY
STAY/NO STAY FOR LUNAR SURFACE OPERATIONS CONFIGURE COMM DAP LOAD 12012 FOR LUNAR STAY LM WT ~.__ AGS LUNAR ALIGN
CSMWT .-~__
BIOMED SWITCH-RIGHT COPY UPDATE
P12 - ASCENTPROGRAM
V47 - INITIALIZE AGS CHECKAPS, RCS, ECS, EP AGS GUIDANCE STEERING END SIMULATED COUNTDOWNAT TIG -1 MINUTE
p&j
AGS PARTIAL POWERDOWN (AGS snvus SW -STBY) CONFIGURESYSTEMSFOR PWRDWN
CLOSEFUEL VENT
PITCH DOWNO.O5"/SEC STOP ORB RATE GO INERTIAL ROLL 170" TO ACQ MSFN V64 ACQUIRE MSFN
DOFF HELMET & GLOVES 1
I
APOLLO 11 ,u,:;(; ]~yrv. -1F
foT)
f :r
DATE
Revision \
A
July
FLIGHT
1 TIME
I 104:oo
8, 1969 PLANNING
I
EAT PERIOD (40 MIN)
L
1
EDITION
1
DOFF HELMET & GLOVES I
EAT PERIOD (40 MIN)
I MISSION
I
- 105:oo
BRANCH
STAY/NO STAY
UPDATE LM ppTi!-q 'LIFT OFF TIMES P22 AUTO OPTICS LUNAR MODULE Tll~~:~j:Q1 (HOR) T2104:39:32 __- __ __ (35") 0.2~~ ( N OR s) N89 LAT + 00.691" __ --LONG/2 t 11.858" _- --ALT - -_001.44--
(IF REQUIRED) UPLINK CMC D SIRED ORIENT m CHANGE)
I If
DAY/REV 5115
NM
PAGE 3-71
FLIGHT PLAN CSM
LM
CMP I
CDR
1830 EDT
.-
MCC-Ii LMP DUMP DSE
rP52 (OPT 1 - PREFERRED GYRO.TORQUE TO DESIRED ORIENTATION FOR PLANE CHANGE (IF PLANE CHANGE IS REOUIRED)
I
.
GDC ALIGN TO IMU F N
1 -
EAT PERIOD (40,MIN)
EAT PERIOD (40 MIN)
CONFIGURELM COMMFOR LUNAR STAY SLEEP VHF A XMIT - OFF VHF A RCV - OFF VHF B XMIT - OFF VHF B RCV - OFF
VHF AM A - SIMPLEX
,CREW STATUS REPORT (RADIATION,
:105:3D
MEDICATION)
CONFIGURE SLEEP STAYION STOW PLSS IN DONNING STATION : 105:38 EAT PERIOD (1 )UR) 1105:44 I
REV 16
REST PERIOD
REST PERIOD
(4 HPURS)
(4 HOIURS)
106:OO
MISSION APOLLO 11 ,.'k‘
EDITION
1
,,( ,‘,Y. ‘ID'1 (c)T) (?J<;\, ;
Revision \
DATE A
TIME
July 8, 1969
105:OO - 106:OO
FLIGHT
BRANCH
PLANNING
1 DAY/REV 5/15-16
PAGE 3-72
FLIGHT PLAN CSM
LM 2330 EDT llo:oo
CMP
MCC-l-l
CDR
MP
1
110:09
I i
i i i i
I 1 1 1
I
I
EAT PERIOD (1 HOUR)
IM i I4 sF ! NI I ; :I ! I
16mm/HCEX/AS PER DECAL 6Omm/FRESH HCFX/ AS 'PER DECAL“'
I-
CHANGE CO2 FILTER
110:40
PREPARATION FOR EGRESS STOW LOOSE ITEMS AND ARMREST PREPARE CAMERAS
Ir
w
j:,T;r) f;:r--
I
1
GET RCS A
B ~-
DESC A-H ASC A-H
I
I 1 lll:oo
1.1:;; -,<-,.v ,I:'/
LM CONSUMABLES UPDATE
PLSS/DPs' DONNING UNSTDW PLSS AND OPS CONFIGURE PLSS AND DPS FOR DDNNIllG
7 APOLLO 11
STAY/ND STAY
-
110:47
I
1
UPDATE LM r CAMERA EXPOSURE UPDATED FOR LM AZIMUTH AND T7 THRU T,O
STAY NO STAY FOR EVA PREP CRE,WSTATUS REPORT (SLEEP, RADIATION)
I
MISSION
DUMP DSE
1
CREW STATUS SYSTEMS PREPARATION FOR EtiRLSS -----C&W LIGHT CK, ADJUST INTERILn711 "GHTING L.
I
I
EAT PERKOD (1 HOUR) COPY 'UPDATE
?I
REST PERIOD (4 HOUR)
I
I
I I
EDITION
DATE
FINAL
JULY 1, 1969 FLIGHT
TIME llo:oo PLANNING
BRANCH
- 111:DD
DAY/REV 5/18
PAGE 3-77
FLIGHT PLAN CMP
MCC-H
LM
CSM 0030 EDT ,-111:oo
LMP
CDR
LMP UNSTOW AND DON OVERSHOES
1:
CDR UNSTOWAND DON OVERSHOES REST 'PERIOD (4 HOURS)
II iATTACH OPS TO PLSS I-
LMP DON PLSS
I: ,I-111:21
-I-
UNSTOW AND CONNECT RCU PLSS SWITCH AND VALVE POSITIONS PREPARE CDR PLSS FOR DONNING
ATTACH OPS TO PLSS CDR DON PLSS
-111:30 CO2 FILTER CHAdGE NO. 9 (11
UNSTOW AND CONNECT RCU
: 111:33
PLSS SWITCH AND VALVE POSITIONS I
INTO A, STORE 9 IN A3) I 02 FUEL CELL PURGE
1111:39 - REV 19
I EAT PERIOD (1 HOUR)
PLSSIEXTRA VEHICULAR C~MM SYSTEM ELECTRICAL CHECKOUT AUDIO SWITCHES CHECK ACTIV TE PLSS COMM SYSTEM
::::A:
(TV C4 B - CLOSE THEN OPEN 5_ r,,n Lln rnllrnUr%IT LqUlrl'ILI'II p:,:p :$z ::;:;;
UNSTOWAND CONNECT OPsx2-HOSE
-
TIME
DATE July
AND ACTUATOR
FINAL SYSTEMSPREP FOR EGRESS CONFIRM "GO" FOR CABIN DEPRESS C/B, VALVES ANU 02/H20 QUANTITY-
8,
111:oo
1969
FLIGHT
PLANNING
BRANCH
- 112:oo
DAY/REV 5118-19
GO/NO GO
PAGE 3-78
FLIGHT PLAN CSM
LM
CMP
EL/25O/BW-BRKT, (f5.6,250,INF),
CDR
INT
CHANGE SHUTTER TO l/125 PITCH UP 38" ROLL 180" TO HEADS UP RO, P320/2zg,YO PITCH DOWN, PHOTOGRAPH LM WHILE TRACKING THROUGH COAS
M S F N
STOP PITCH AND ROLL 180" TO HEADS DOWN ATTITUDE FOR SURFACE ' OBSERVATIONS STOP CAMERA
LMP
SELECT DEPLOY SITE CARRY CAMERAS DEPLOY LR3 EXPERIMENl PHOTO EXPERIMENTS
SELECT DEPLOY SITE CARRY EXPERIMENTS DEPLOY PSE TAKE CLOSEUP PHOTOS
DOCUMENTEDSAMPLE COLLECTION -___ REST/PHOTO LMP CLOSE-UP PHOTOS TETHER SAMPLE BAG TO LMP PHOTO SAMPLING UNSTOW GNOMON PHOTO DS AREA PHOTO SAMPLE COLLECTION STOW ALSCC FILM COLLECT ENVIRONMENTAL SAMPLES RETRIEVE AND STOW SWC PACK SRC CLOSE AND SEAL SRC
JOCUMENTEDSAMPLE COLLECTION MOVE BULK SRC TO STRUTS OR FOOT PAD PREPARE DS SRC
REST/PHOTOLMF
TRANSFER BULK SRC AND
\
s R180, P282/185, YO HGA P -7, Y 183
STILL CAMERA MAGAZINE REST CHECKEMU TRANSFER DS SRC I
MISSION APOLLO 11 [()T)
(.jr... :- \
COLLECT CORE TUBE SAMPLE UNSTOWTOOLS COLLECT SAMPLES STOW ALSCC FILM COLLECT ENVIRONMENTAL SAMPLES COLLECT LOOSE MATERIAL CORE TUBE SAMPLE
1+30
1t40 DUMP DSE
1+50 .M ACQUISITION ;ET:
2+00
2+10
SRC TRANSFER
)"rf,(: ),‘rr,., :I".,
MCC-!-I
,
DATE
EDITION &vision
/
A
July
TIME
8, 1969 FLIGHT
EVA TERMINATION WIPE SU T ANEFEMU WIPE FELT ON LANDING PAD AND LADDER ASCEND LADDER INGRESS CABIN CHECK LM OPERATE SEQ CAMERA RECEIVE AND STOW SRC AND MAGAZINE RECEIVE AND STOW SRC
PLANNING
114:00-115:oo BRANCH
1 DAY/REV 5/21
2+20
2t30
PAGE 3-81
FLIGHT PLAN MCC-H
LM
CSM 0430 EDT -115:oo
CMP PRESLEEP CHECKLIST CREW STATUS REPORT RADIATION, MEDICATION) CYCLE 02 & Hp FANS CHLORINATE WATER : WASTE MNGMT OVBD DRAIN VLV - OFF WASTE STOW VENT VLV CLOSED EMER CABIN PRESS VLV BOTH SURGE TANK 09 VLV - ON REPRESS PACK'02 VLV-OFF POTABLE H20 HTR - OFF SELECT COMM NORMAL LUNAR CONFIGURATION - EXCEPT: S-BAND SQUELCH ENABLE HGA TRACK - REACQ HGA BEAM - NARROW HGA P -59, Y 355 -
LMP
CDR TERMINATE EVA WIPE FEET ON LANDING PAD AND LADDER ASCEND LADDER ---I-
lr 17
CABIN REPRESS 1:
JETT EQUIP L CLOSE FWDHATCH
2+40 END EVA
POST EVA SYSTEMS CONFIGURATION CAUTION LIGHTS OFF
IT 'I
2+30
DISCONNECT RCU
115:18
DISCONNECT OPS 02 HOSES CONNECT LM 02 HOSES CONFIGURE VALVES AND CIRCUIT
BREAKERS
DISCONNECT PLSS H20 HOSES 1
SWITCH TO LM COMM SYSTEM
115:30
- 115.37 -REV
M S F N
I
PLSS/OPS DOFFING REMOVE LMP RCU OPS CHECK STOW PLSS/OPS ON CABIN FLOOR
I EAT PERIOD ('
REMOVE CDR RCU STOW PLSS/OPS ON CABIN FLOOR
6 FRAMES EACH, FAR & NEAR FIELD (FOCUS 50' & 20') AND 80mm/BW/EVA CARD iyl 6 FRAMES EACH, FAR & NEAR
nus
H"/IR)
t
;O’ &,10’)
PREP JETW -____.-FOR EQUIiMENT - .-
COPY REPORT
REPORT PLSS FEEDWATER
L
)"r:;t: Irl‘~,
]",
116:OO
MISSION
EDITION
APOLLO 11
Revisicn
(,!T)
fl!r;
:
1
REMOVE OPS,FROM PLSS
1
DATE A
July
TIME
8, 1369 FLIGHT
PLANNINS
115:00-116:00 BRANCH
DAY /REV 5/20-21
PAGE 3-82
-
UU
5, L-----
FLIGHT PLAN MCC-H
LM
CSM 1130 EDT 122:oo
CMP
LMP
CDR
LGC SELF TEST
: :
CREW STATUS REPORT (SLEEP:
i
I
:
SELECT COMM: NORMAL LUNAR CONFIGURATION CREW STATUS REPORT(SLEEP)
.
AGS TURN ON, SELF TEST AND SYSTEM TESTS INITIALIZE AGS TIME REPORT BIAS TO MCC-H REPORT: P57 - GRAVITY AND ONE CELESTIAL BODY (REFSMMAT) N04: ---.--N71: -N93: X - -f --" I
GET
?.R- ON, SELF TEST, OFF
M s L :
122:30 122:31
---.
--.---
-
T’--
--
:
AGS GYROCALIBRATE
RCS HOT FIRE
I
L
COPY TIME BIAS
M S F N
!: 122:37 V45 RESET LUNAR SURFACE FLAG
:-
P52 IMU REALIGN OPTION 3 (REFSKMAT) REPORT P52 LIFT OFF REFSMMAT
EAT PERIOD (35 MIN)
EAT PERIOD (35 MIN)
IJPL'..NK LGC ,M STATE VECTOR ISERTION +18 MIN
N71: N05: N93: X Y 123:00
Z GET: -
-
-:-
APOLLO 11 br:;L‘ F'C1‘,,..i1p 1 (f T) ji:r;r
DATE
iDlTlON
--:-
<evision
I i
‘I
I
A
July
0,
TIME 122:00
lrL9
FLIGHT
PLANNING
- 123:00
BRANCH
DAY /REV b/24
PAGE 3-88
FLIGHT PLAN MCC-H
LM
CSM 1230 EDT 123:00
CMP
LMP
CDR
UPDATE LM IASCENT PAD LCSI PAI CONSUMABLES UPDATE (A FROb! NOMINAL)
COPY ASCENT PAD LOAD PAD DATA
COPY CONSUMABLES UPDATE
AGS: AZIMUTH CORRECTION = 0 H = 60,000 FT H DOT = 32 FPS NO S-BAND YAW MNVR ORBIT INSERTION MODE
123:lO
GET: RCS TOT _ A B C
SET CAMERA FOR ASCENT 16mm/HCEX/OVERHEAD (f4,500,INF) 12 fps
I 123:24
D H2 TOT O2 TOT
RR XPONDER- SELF TEST THEN PNR
COPY CONSUMABLES UPDATE
-123:30 REV 25
02 FUEL CELL PURGE
SET UP CAMERA FOR DOCK11 16mm/l8/CEX-BRKT MIR(f8,250,INF) 6 fps
-I
REPORT: P57-GRA' VITY AND ONE Briny (T-ALIGN) CELE3TIi.bLII I__ N04: --_.N71: -N93: X _ -.-Y
__.---
z
-----
GET:
_---
LM CONSUMABLES UPDATE GET' ---I:RCS A DESC O2 DESC A-H
ASC A-H ' -:-
123:56
3 MISSION
EDITION Revision
1
APOLLO 11 by;'; ,,11^,, /]:,e
f(;;)
(:c:
124:00
;
ENTERAGS LUNAR ALIGN
+
TIME
DATE A
July
8, 1969 FLIGHT
123:00-124:00 PLANNING
BRANCH
I DUMPDSE
DAY/REV
PAGE
6124-25
3-89
FLIGHT PLAN CSM
MCC-H
LM 1330 EDT 124:OO
CMP V64 ACQUIRE MSFN VHF RANGING MNVR TO LIFT OFF RO, P250/207, YO
CDR
LMP
LOAD DAP - 12012 DON HELMET AND GLOVES L;;',;""'"' PROGRAM
DON HELMET AND GLOVES
PRELAUNCH SWITCH CK (PREI RESTRAINTS APS i
UPDATE LM p2cmm-
GO/NO GO FOR PGNCS ASCENT GUIDANCE AND LIFT OFF THIS REV PRELAUNCH SWITCH CK RESTRAINTS
LIFT OFF -6 MIN DISABLE S-BAND RELAY
LIFT OFF COMM START 16mm CAMERA
EXT RNDZ LT - ON
V47 INITIALIZE TIG-5
PITCH DOWN, O.ZO/SEC
SEC, ABORT STAGE APS, LIFT OFF
II”.
AGS
II-7.Ld.L”
BT: 7 RR LOCK ON, MODE II CONFIRM INSERTION
124:30 124:31
VHF RANGING REPORT: -~~--P52 (LIFT OFF REFSMMAT) N7,. OPTION 3 --)-.-N05: ----*--
~.-jORBIT
RR-OFF 1NSERTION VEL
124:36 124:37
ECS CHECK V48 LOAD DAP N46. 12002 V56, V41 TURN ON TRACK LIGHT
JO5: i93 :
-
-_*_
_
X
-
-.-
_
--*--__
Y
--------
;ET
---*----
--
P
-
-
_
-:-
D73 --
_
-:-
,-CT ..-a
1
APOLLO 11
(C)T) (Nov i:')
EDITION Revision A
I
DATE
I
TIME 124:OO - 125:OO
July 8, 1969 FLIGHT
A-Y ”
b
CSM: RO, P235/119, -I
125:OO
‘MISSION
DD!TWDIICT .I-.....14.
I
_
RR - ON
-----
&;I: Form ?lh'l
--_
Yo
_~ v93 (BEFORE FIRST MARK) V80, V47 INITIALIZE AGS
-..
PLANNING
BRANCH
1 DAY/REV 6125
YO
\:
IRO, P257.3,
LM FDAI:
Y
X
GET
RO, Pw/207,
P52 (LIFT OFF REFSMMAT) ,,7,: OPTION 3
/
N93:
2
INSERTION
1
PAGE 3-90
YO
FLIGHT PLAN
NOTES
EQUIPMENT STOWAGE
VACUUM PGAS
131:18
1 Ii-
131:25 REV 29
SET UP CAMERA FOR LM JETTISON 16mm/l8/CEX-BRKT,MIR (f8,750,7) 12 fps
DAP CONFIGURATION FOR LM JETTISON CSM, 0.5' DB, 0.5'/SEC A/C ROLL, 4 JET
SM RCS CHECK ENABLE JETS 8-3 AND C-4 CONFIGURE DAP - Rl=lllOZ, GO/NO-GO FOR PYRO ARM
R2=11111
GO/NO GO
i
DUMPDSE
1
!I!I
132:OO
MISSION
DATE
EDITION
1
Revision
APOLLO 11 YSC Form 29 (uay
RO, P45/25, \ HGA P-53, Y3
se)
A
July FLlOHl
I
8, 1969 PLANNINO
TIME 131:00
BUNCH
- 132:00
DAY/REV
PAGE
6129
3-97
_
MCC-n
FLIGHT PLAN
2130 EDT 132:00
NOTES’
MNVR TO TEI BURN ATTITUDE (EXCEPT ROLL) V66 - TRANS CSM STATE VECTOR TO LM SLOT BURN STATUS REPORT RECORD PRELIMINARY TE130 MNVR PAD
UPDATE piypimm
GO INERTIAL DOFF AND BAG PGA'S HELMETS AND GLOVES
1L
Y13.8 R1.l P i.2152.6 HGA P -79,Y 10
132:23
132:30
1
EAT PEI
EDITION
MISSION APOLLO 11 USC Form 29 (yay
Revision 99)
I A
ID
DATE
I
.July 8, 1969 FLlOl41
WANNINO
TIME 132:00
BRANCH
- 133:00
DAY/REV 6/29
PAGE 3-98
-
TEI BURN CHART
P OR Y RATES TEI
ATT DEVIATION
loo/SEC TAKEOVER
+10" TAKEOVER
SHUTDOWN TIME BT + 2 SEC &
AV, = -40 FPS
RESIDUALS
TRIM X AXIS TO 0.2
FPS
TEI ABORT MODES BT
TEI VGo
TRAJECTORY
ABORT MODE
I
o-01:3 0 LUNAR ORBIT MODE III
3292.7
- 1436.0
1436.0
- 1207.0
1:30-
1207.0
- Q
1:40-02:2 9 UNSTABLE/
1:4 10 UNSTABLE
MODE II
MODE
HYPERBOLIC
I
3-1 OOa
- AFTER 1 REV - 2 SPS BURNS FOR ORBIT STABILIZATION AND WATER OR CLA LANDING. I - 1 BURN AT TEI + 2 HRS P37 AT SPHERE OFINFLUENCE HYPERBOLIC (Av 580 to 0, BT ;;;;; -
Revision
A
FLIGHT PLAN 194:oo (EI -1 HR)
NOTES
PRIMARY EVAPORATOR ACTIVATION FINAL GDC DRIFT CHECK TERM CM RCS PPFHEAT SECONDARY CVAPORATOR ACTIVATION PYRO BATTEKY CHECK RECORD ENTRY PAD AND RECOVERY DATA
UPDATE p!KF
P27 UPDATE - V66 - TRANS CSM STATE VECTOR TO LM SLOT
:20 UPLINK (CSM
SET DET TO RRT EMS INITIALIZATION RSI ALIGN TO GDC CM RCS CK ENTRY BATTS - ON
194:30 (EI -30
SEPARATION CHECKLIST GO FOR PYRO ARM
GO FOR PYRO ARM
P61 ENTRY PREP MNVR TO CM/SM SEP ATT
L
ICM/SM SOP]
:5D
P62 - ENTRY ATTITUDE
1
MNVR TO ENTRY ATT
195:oo
MISSION
1
APOLLO 11 YSC Form 29 (#a~ 89)
DATE
EDITION FINAL
I
JULY 1, 1969 fLlOnT
WANNINO
TIME
I 194:oo BRANCH
- 195:oo
1 DAY/REV 9/TEC
PAGE 3-134
FLIGHT PLAN
MCC-I
P63 - ENTRY INITIATE IEI - GET = 195:05:04 1 P64 - ENTRY POST .05G
:lO TIME FROM ENTRY INTERFACE MIN:SEC
TRAJECTORY EVEN1
: 20
-
0o:oo
400,000 FEET (GET 195:05:04) ENTER S-BAND BLACKOUT 0.05G KA - INITIATE CONSTANT DRAG RDOT = -700 FPS PEAK G (6.6) SUBCIRCULAR VELOCITY P64 to P67 EXIT S-BAND BLACKOUT GUIDANCE TERMINATION DROGUE DEPLOYMENT MAIN DEPLOYMENT SPLASHDOWN
195:30
:40
L/D = 0.295,
y = -6.50",
00:18 00:28 00:52 01:18 01:22 02:08 02:OB 03:24 07:14 08:12 09:oo 13:55
V = 36,195,
& R = 1285
:50
L
196:00
MISSION APOLLO 11 YSC Form 29
DATE
EDITION (May 69)
Revision
A
July FLlOHl
8, 1969 WANNINO
TIME 195:OO - 196:00 BIAMCH
DAY /REV
PAGE
9/TEC
3-135
TO
:
FROM
: CF/Chief,
SUBJECT:
Revision
DATE:
Flight
Crew
A to the Apollo
Flight
8, 1969
In reply refer CF3&2-9M-133
Division
11 Final
July
to:
Plan
Enclosed is Revision A to the Apollo 11 Final Flight Plan. Enclosure 1 contains the pen and ink changes to be made on the indicated pages. Enclosure 2 contains the new pages which replace the same numbered pages in the final edition of the flight plan. Changes on the new pages are made with prestige elite type rather than gothic type so they will be readily evident.
Enclosures
2
CF342:TAGuillory:jat
7-E-69
Buy U.S. Savings Bonds Regularly on the Payroll Savings Plan
ENCLOSURE 1 MAKE THE FOLLOWING PEN AND INK CHANGES TO THE FINAL FLIGHT PLAN CHANGE
PAGE 1-7
ON "LM POWEREDDESCENT/HIGH GATE TO TD" FIGURE CHANGE ORDINATE AND ABSCISSA FROM "FT" TO "FT X 103"
l-10
ON TABLE l-3
FIRST COLUMN CHANGE "1409
ON TABLE l-4
CHANGE Al LONGITUDE FROM 60.500"E
-
1-11
CHANGE Gl DELTA ALTITUDE FROM -001.97
1-17
PARAGRAPH Ei, CHANGE TIMES: 103:30:00-TO 107:15 148:00:00 TO 151:00 154:00:00 TO 172:00
2-31
& 2-32
2-44
CHANGE TITLES
EDT" TO "1209
EDT"
TO 65.50Q"E
TO -001.76
FROM "PHASING" TO "ASCENT PHASING"
CHANGE 275 (+0418.1)
TO 275 (tO418.5)
CHANGE AVX, AVY, AND AVZ BLOCKS FROM 00 0 - -*TO 00 ----2-48
CHANGE AVR N42 BLOCKS FROM + 0 CHANGE F/A, TO 00 ----
R/L,
0
AND D/U BLOCKS FROM 00
CHANGE "S-IVB
TO ORBIT CAPABILITY"
TO + 0 ----0 ---
3-ii
AT 05:25
TO "CO1 CAPABILITY"
3-l
AT 00:37 CHANGE "ECS REDUNDANT COMPONENTCHECK" TO "SEC GLYCOL LOOP CK" AT 00:43 IN BOTH COLUMNS CHANGE "RECORD AAZ CORRECTION" TO "RECORD Z TORQUE"
3-5
AT 04:07
DELETE "THRUST MONITOR - P47"
AT 04:52
DELETE "MANEUVER TO OBSERVE SLINGSHOT"
3-6
AT 05:lO
IN MCC-H COLUMN "ADD
3-10
AT 11:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "MCCl WILL BE DELAYED TO MCC2 IF PROPELLANT COST IS NOT PROHIBITIVE"
3-19
AT 26:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "TO AVOID EXECUTION OF MCC3, A NON FREE MCC2 WILL BE EXECUTED (SPS BURN IF THE BT >3 SEC)"
1
------
.-__
--~
UPLINK CMC 1 ZERO TRUNNION BIAS”
CHANGE
PAGE 3-33
AT 53:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: "MCC3 WILL BE DELAYED TO MCC4 IF PROPELLANT COST IS NOT PROHIBITIVE"
3-43
AT 70:50 IN NOTES COLUMN CHANGE THE MCC NOTE TO READ: BE EXECUTED WITH THE SPS IF THE BT >3 SEC"
3-44
AT 71:25 DELETE "PRE-LO1 ECS REDUNDANT COMPONENTCK ACTIVATE PRIMARY EVAPORATOR" AND ADD "SECONDARY RADIATOR LEAK CHECK"
3-51
AT 80:12
CHANGE "DO NOT TRIM" TO "TRIM X AXIS TO 1 FPS"
3-53
AT 82:13
CHANGE R 0,
3-54
AT 83:20
CHANGE R 82, -350/229,
3-61
AT 95:00
ADD "ROLL RT 40",
3-63
AT 96:48
IN MCC-H COLUMN DELETE "BLOCK DATA"
3-73
& 3-74
P -257/297,
Y 0 TO R 0,
P 296/303,
Y 0
Y 0 TO R 82,
P 296/229,
Y 0
TO R 122,
P 229,
Y 0"
DELETE LOCAL HORIZONTAL PITCH OF 166.3 107:14 RESPECTIVELY
& 244.2
3-76
AT 109:45
IN LM COLUMNS ADD "RADIATION
READOUT"
3-79
AT 112:30
IN CMP COLUMN ADD "ACTIVATE
3-83
AT 116~40
IN LM COLUMN ADD "CONFIGURE COMM (TV-OFF)"
3-91
AT 126:00
IN MCC-H COLUMN ADD "DUMP DSE"
3-92
AT 126:07
IN LMP COLUMN CHANGE P -58 TO P +58
AT 106:47
AND
PRIM EVAPORATOR"
AT 126:30 CHANGE CSM ATTITUDE FROM R 180, TO R 0, P 239/160, Y 0 3-93
"MCC4 WILL
P _264/177,
Y 0
AT 128:00 ADD IN CMP COLUMN "EXT RNDZ LT - OFF" AND IN MCC-H COLUMN "DUMP DSE" AT 127:00
IN CMP & MCC-H COLUMNS ADD "GO/NO GO FOR PYRO ARM"
3-95
AT 130:00
IN MCC-H COLUMN ADD "DUMP DSE"
3-100
AT 134:12
DELETE "ECS REDUNDANT COMPONENTSCK"
3-101
AT 135:18 R2=lllll"
CHANGE "DAP - Rl=lOlll AND MOVE TO 135:05
3-102
AT 136:15
ADD "DEACTIVATE PRIM EVAPORATOR"
3-132
AT 192:27
CHANGE "MENKAR (07)
2
R2=11111"
TO "DAP - Rl=lOlOl
ENH" TO "MENKAR (07)
EFH"
ENCLOSURE 2 SYMBOL NOMENCLATURE
ff
l--
LUNAR PENUMBRA (OCCURS PRE LOI,)
PENUMBRA(PRE EI)
ALSO EARTH
SPACECRAFT SUNSET
.
M S F r?
b 4---
MADRID 85FT DISH COVERAGE DARKNESS (UMBRA) MSFN LOS
I:--!
.
SPACECRAFT SUNRISE LUNAR PENUMBRA (OCCURS PRE LOI,)
ALSO EARTH
PENUMBRA(PRE EI)
-3 c---LUNAR
IMSFN
SURFACE
AOS
HONEYSUCKLE85~~ DISH COVERAGE j_cGOLDSTONE
85FT DISH COVERAGE
LUNAR TERMINATOR SPACECRAFT SUNSET
DARKNESS
+-LUNAR
TERMINATOR
xi
Revision
A
INTRODUCTION This Flight Plan has been prepared by the Flight Planning Branch, Crew Division, with technical by TRW Systems. This document schedules the AS-506/CSM-107/LM-5 to fulfill, when possible, the test objectives quirements, G Type Mission Lunar Landing.
operations defined in
The trajectory parameters used in this Flight Plan launch, with a 72" launch azimuth and were supplied Analysis Division as defined by the Apollo Mission Trajectory.
Flight
and crew activities the Mission Re-
are for July 16, 1969 by Mission Planning and G Spacecraft Operational
The Apollo 11 Flight Plan is under the configuration control of the Crew Procedures Control Board (CB). All proposed changes to this document to the CB via that fall in the following categories should be submitted a Crew Procedures Change Request: 1.
Items
that
impose
additional
2.
Items
that
impact
the
3.
Items
that
result
in a significant
4.
Items that day in the
result Flight
in moving Plan.
5.
Items that
require
The Chief, Flight fall in the above
training
accomplishment
a change
Planning Branch categories.
Mr. T. A. Guillory will act the Apollo 11 Flight Plan.
crew
major
or impact
of detailed
test
RCS or EPS budget activities
to the
flight
as co-ordinator
change.
all
activity
file.
determine for
what
proposed
proposed changes
Any requests for additional copies or changes to the distributicn this document must be made in writing to Mr. W. J. North, Chief, Division, MSC, Houston, Texas.
xii
procedures.
objectives.
to a different
data
(FCSD) will
crew
lists Flight
changes to of Crew
b.
The coolant loop operation will be as follows: Launch - primary loop operation (1) Earth Orbit - primary loop operation and secondary (2) loop test Post TLI - deactivate both evaporators (3) Pre LO1 set rad leak ck only. (4) At 112:30 activate primary evaporator (5) Post TEI - deactivate primary evaporator (6) Entry interface minus 1 hour - activate primary and (7) secondary evaporator.
3.
Guidance and Navigation a. During lunar orbit, the CSM and LM will utilize the same landing site REFSMMAT such that the gimbal angles would be O,O,O at landing with the LM sitting face forward on landing site number two and the CSM over the landing site pitched up 90" from local horizontal "heads up". b. During PTC the CSM/LM x-axis is Ditched up 90" (North)%A for TLC and down 90" (South) for TEC with the Y-Z axes This change in x-axis in the plane of the ecliptic. pointing is to enable simultaneous viewing of the earth and moon through the side windows while maintaining a favorable hiqh aain antenna oosition. c. The CSM tracking light will be on continuously from undocking to landing and from LM lift-off to docking.
4.
Landmark Tracking The following ground rules were used for landmark tracking. a. IMU to be realigned on the dark side preceding each tracking period. b. MSFN is reacquired after each tracking period. The tracking data will be acquired by MSFN after all the marks have been made and while N49 (hR,hV) is displayed. MSFN will give a GO when data acquisition has been verified. c. The pseudo landmark tracking (Al) will be used to determine the altitude of an area in which the LM will be making altitude checks after DOI. The data will be processed during the sleep period after the trackings and relayed to the LM prior to undocking.
1-18
Revision
A
d.
e.
f.
F.
In the docked configuration the CSM/LM approaches the landmark in an inertial hold attitude. This inertial attitude + places the spacecraft 2" below the local horizontal at the 35" elevation angle point. At 35" elevation angle a pitch down of 0.3"/sec is initiated. Five marks are then taken with the time between marks a minimum of 25 (See tracking profile) seconds. In the undecked configuration the CSM approaches the landmark in ORB RATE and. pitched down 22" from the local horizon- ' tal. At 35" elevation angle five marks are taken with the time between marks a minimum of 25 seconds. ORB RATE is continued throughout the marking period. In the undecked COAS tracking the CSM will approach the LM in ORB RATE heads up and pitched down 40" from the local horizontal. When the LM is centered in the COAS the CSM will initiate a variable pitch rate to keep the LM centered in the COAS.
MZO
v
es
\\,i
HY+k
,' \
9
,;c
q\ -------Q &<
I
5.
CSM/LM and CSM attitude maneuvers will normally be at a rate of 0.2"/sec or 0.5"/sec. unless other rates are required. NOTE: At 0.2"/sec,15 minutes is required to maneuver 180". At O.S"/sec, 6 minutes is required to maneuver 180".
6.
ive thermal control mode will be initiated after MCCl or as soon as MCCl is scrubbed and maintained throughout the mission (except in lunar orbit) until at least three hours before entry except for interruptions for midcourse corrections, communications orientation (maximum interruption of three hours). PTC will not be initiated before approximately 7:00 GET.
7.
Service Propulsion System All SPS burns will on Bank A except LO11 which will be initiated
be initiated on Bank B.
LM Notes 1. Entries into the LM a. Three entries into the LM are scheduled in the at 56:30, 81:30 and 95:52 GET respectively.
1-19
timeline
FLIGHT PLAN 1730 EDT
CMP
LMP
CDR
CLEAR TUNNEL OF CM HATCH INSPECT TUNNEL & DOCKING LATCHES REMOVE PROBE & DROGUE
_-.. -
TEMPORARILY STOW PROBE AND DROGUE
:lO
TRANS TO LM PWR
CSM PWRTO LM - ON (AT LMI' REQUEST)
-
ACT VHF B FOR DATA XMIT FOR 5 IMINUTES
:20
-TRANS TO CSM PWR
DUMP DSE (LM DATA) IVT TO LM
PWRTO LM - OFF (AT LMP KEQUOST)
-
OPERATION OF LM 16mm CAMERA
:40 LM FAMILI
-
L
’ MISSION APOLLO 11 f:;T)
(:Tr.,, :
l&vision
(IZATION
LM FAMIL
lIZATION
:50
57:oo
DATE
EDITION j
ASSIST CDR
L 56:30
PTC
I;~?,T; 21"'
.~~
OPEN LM HATCH RECORD ROLL CAL ANGLE IVT TO LM
CONFIGURE DSE TO RECORD LM DATA
":;I:
MCC-H
LM
CSM
A
July
8, 1969
-__ FLIGHT PLANNING
TIME 56:00
- 57:00
BRANCH
DAY/REV 3/TLC
PAGE 3-35
-
T
LOI, BURN CHART
LOI,
P OR Y RATES
ATT DEVIATION
loo/SEC TAKEOVER
+lO" TAKEOVER
SHUTDOWN
PESIDUALS
TIME BT + 10 SEC
DO NOT TRIM
LOI, ABORT MODES
2924.0
TRAJECTORY
'GO
BT
- 2129.0
O-01:50
Lo1l
2129.0
- 1589.0
1589.0
- 0
01:50 03:oo
03:;;
is
HYPERBOLIC
ABORT MODE MODE MODE II
(UNSTABLE
LUNAR ORBIT
MODE III
3-46a
I - COAST 2 HR - OPS - P37 (P37 BEYOND SPHERE FOR VGO >2279 AND BT <01:3( - COAST 2 HR - 2 DPS BURNS FOR STABILIZATION AND bfATEt? or CLA LANDING - DPS BURN AFTER ONE REV
Revision
A
2130 EDT
MCC-I4
_ -
84;O0 84:Ol
FLIGHT PLAN
NOTES
l-
j 02 FUEL CELL PURGE
5M PRESiEEP CHECKLIST CREW STATUS REPORT ,\, (RADIATION & MEOICATION) ,YCLE 02 & H2 FANS IHLORINATE POTABLE WATER SELECT NORMAL LUNAR COMM CONFIGURATION - EXCEPT: S-BAND SQUELCH-ENABLE HGA TRACK-REACO HGA BEAM - NARROW IIERIFY: WASTE MNGMT OVBD DRAIN-OFF WASTE STOW VENT-CLOSED EMERGENCY CABIN PRESS-BOTH SURGE TANK 02 VALVE-ON REPRESS PACK 02 VALVE - OFF POTABLE WATER HTR-OFF iL LM TUNNEL VENT VALVE-LM PRESS
1 REV 5
;
84:30
-
84:33
EAT PERIOD
'02
FILTER CHANGE NO. 7
9 INTO A, STORE 7 IN B6
MISSION
1
EDITION
APOLLO 11 YSC Form 29 (yay
FINAL 69)
DATE
I
JULY 1, 1969 fLlOn1
RINNINO
TIME 84:00
BUANCH
- U5:OO
DAY/REV 4/5
1 PAGE 3-55
LUNAR ORBIT REST PERIOD ATTITUDE
LOCAL HORIZONTAL
I LOS EARTH 3-55a
Revision
A
FLIGHT PLAN MCC-H
LM
CSM 1130 EDT
CMP
LMP
CDR
98:00
MANEUVER TO TRACKING ATTITUDE R 0 ,P297/27O,YD DOFF HELMET & GLOVES 98:21 SELECT OMNI C
DON HELMET & GLOVES
DON HELMET & GLOVES
ARS/PGA PRESSURE INTEGRITY CHECK
ARS/PGA PRESSURE INTEGRITY CHECK
CABIN REGULATOR CHECK
CABIN REGULATOR CHECK
DOFF HELMET & GLOVES
DOFF HELMET & GLOVES
COPY DAP DATA COPY GYRO TORQUE ANGLES AND FINE ALIGN IMU
SELECT OMNI -FWD BIO MED SWITCH - RIGHT
X
98:30
) z
, Y
GO INERTIAL UNSTOW OPTICS P22 ORBITAL NAVIGATION
UPDATE LM DAP DATA GYRO TORQUE ANGLES
OPT:ICS LMK ID 130 T1 9 8: 4 0: 0 2 (HOR) T2 1yr.4 5.08(35") 4.6 NM @i%g'--mRATE GYRO CHECK
4GS ACT & SELF TEST
N 89 LAT +ocl.2 4 LONG/Z + 11..8 4 ALTITUDE- ,o 0 l..A&NM
RO,P126.5/22.5,YO CONTINUEPITCH TO AGS CAL PITCH ATT (22.5)V64 ACQUIRE IdSFN ANT P 187, Y 70
V64 ACQUIRE MSFN
MISSION )Gp','; j:r,lrr,
1
EDITION
Revision APOLLO 11 'IF,, (c)T) (:j<-: I:)
DATE
I A
July
8, J9hY FLIGHT
TIME
I 98:00 PLANNING
- 99:00
BRANCH
DAY/REV 5112
DUMP DSE
PAGE 3-65
I
3 4
1
FLIGHT PLAN CSM
LM 1230 EDT 99:oo
CMP STOW FLIGHT PLAN UNSTOW SOLO BOOK COPY PADS
MCC-H
CDR
LMP
UPLINK LGC
DRIFT CHECK-REPORT GIMBAL .ANGLES & TIME TO MSFN DEPLOY LANDING GEAR
I VECTORS LGC/CMC CLOCK SYNC PIPA BIAS LGC ABORT CONSTANT
ORDEAL INITIALIZATION LOAD DAP DATA - 32012 CSM WT -P TRIM Y TRIM DPS GIMBAL DRIVE AND THROTTLE TEST
DON HELMET & GLOVES SC CONT - SCS MIN/MAX DB, LOW/HIGH RATE (AT REQUEST OF CDR) GO/NO-GO FOR UNDOCKING DISABLE ROLL JETS FOR RCS HOT FIRE
V47 INITIALIZE
AGS
COPY AGS ABORT CONSTANT AND K FACTOR
RCS PRESSURIZATION
RCS PRESSURIZATION
m
/f%%%&r UPDATE CSM
GO/NO-GO FOR UNDOCKING RCS CHECKOUT
RCS CHECKOUT
TUNNEL VENT VALVE - OFF RECORD LM PCM DATA
SC CONT - CMC AUTO MANEUVERTO ACS CALIBRATION ATTITUDE
SC CONT - SCS RATES
MISSION APOLLO 11
1‘, . 1.I-.,.,,, 11s;I) i ( T ) (. T,..;
:99:49 - REV 13 r
1
EDITION Revision A \
DPS PRESS &; CHECKOUT
DATE July b,
TIME lYh9
F'LIGHT
99:oo PLANNING
- loo:oo
BRANCH
DAY/REV
PAGE
5/12-13
3-66
FLIGHT PLAN 1330 EDT -100:00
CMP RR TRANSPONDER ACT & SELF TEST CONFIGURE DAP GDC ALIGN TO FOR UNDOCKING, CSN ONLY Rl = 11102 R2 = 11111 SC CONT - SCS START 16HM CAMERA -mOCKI
I
MCC-H
LM
CSM
LMP
CDR DAP DATA LOAD
V47 AGS ALIGN
21112
CSM: R 0,
II DON HELMETS AND GLOVES PREPARE FOR UNDOCKING
ENABLE 83 & C4 RCS JETS V64 ACQUIRE MSFN LM INPECTION, CAMERA OFF
'AW LEFT 60", )ET ORDEAL 'AW 360".
P15 /14, /'<'
RO, P194, Y60 JPLrNK LGC
PITCH UP 110" ACOUIRE MSFN ANT P 123, Y -37
LM INSPECTION
DOFF HELMET & GLOVES COPY PADS CONFIG FOR
DESCENT TARGET LOAD PIPA BIAS
SC CONT - CMC CSM VOICE P30 EXT A’/ P41 RCS THRUSTRELAY
?
SEPARATION
c
100:48
P20 AUTO MANEUVER SXT & VHF RANGING
JPDATE LM DO1 MNVR PAD PDI PAD i PDI ABORT
;;o;;;gEsT
JPLINK LGC CSM STATE VECTOR (5)
LM E:
JPDATE LM piGp&m
100:54 VHF RANGING RR - OFF COPY PA0
i
.q,.,.
,.
.!
APOLLO 11 I I. \, i ,
DATE
EDITION
MISSION
Kevisior.
j
UPDATE CSM IrtUE
101:oo
A
July
TIME
8, 1969 FLIGHT
100:00 PLANNING
- 101:oo
BRANCH
DAY /REV 5113
PAGE 3-67
PAD
FLIGHT PLAN MCC-H
LM
CSM 1430 EDT 101:oo
CMP P52 IMU REALIGN OPTION 3 REFSMMAT REPORT:
LMP
CDR
REPORT: P52 (LDG SITE REFSMMAT) N71: _
--)
-.. -~
LM STATE VECTOR
N05: -_-.-N93 :
I M S
X Y _
k
z
UPLINK CMC
SYSTEMS CHECKS
_.-
--
-
_.--
-
-
_ _'--GET -----
DUMP DSE
V47 AGS ALIGN
--
GO/NO GO FOR DO1
P40 DPS THRUST MNVR TO DO1 ATTITUDE
UPDATE LM STEERABLE ANTENNA ANGLES (GET: To2:19)
OMNI AFT, PCM LBR VHF A-VOICE, B-DATA GDC ALIGN TO IMU VHF 6 - DATA P20 AUTO MANEUVER TO SEXTANT TRACK LM
1:
CONFIRM DOI-VHF RANGING INCORPORATE P76 P20 AUTO MANEUVER TO SEXTANT TRACK LM SEXTANT TRACK ONLY
101:30
SLEW STEERABLE ANTENNA CSM: RO, P215/319,YO ANT P 220, Y 28 -
- 101:41
DPS,DO ULLAGE: 2 JET, BT: 28.5 SEC
TRIM Vx RESIDUALS PITCH DOWN, P=195, RR-01 P20 MAN LOCK - ON
- 101347
- REV 14
ORUIT 8.97 RR-OFF i'%J tXl
SEXTANT'AND VHF TRACKING OF LM 102:oo
IMISSION APOLLO 11 by ,,,- ,.:,,
1' / ,.>T!
1
EDITION Revisiun A
i 1~\. 8' '
TIME 101:oo
1969
FLIGHT
PLANNING
SEC
X 57.87
LM FDAI: VHF A-VOICE/RNG __~.~~ . VHF B - XMTR - OFF SET CAMERA 16mm/HCEX(4,500,INF) 6 fps COAS OVERHEAD
AV
LOAD PDI + 12 ABORT PITCH DOWNTO 106.5' YAW LEFT 180"
DATE July 8,
7.5
- 102:oo
BRANCH
DAY /REV 5/13-14
RO, P294.9, <
PAGE 3-68
Yo
FLIGHT PLAN CSM CDR
CMP 7-
LMP
P52 PITCH ALIGNMENT CHECK
SEXTANT AND VHF TRACKING OF LM
RR - ON P20 MODE II
V06N20, ENTER ON MARK RECORD PITCH CDU N22, REOCRD PITCH CDU BATTERIES 5 & 6 ON
LOCK - ON
SYSTEMS CHECK DPS, OPS, RCS, EPS, CWEA
TERMINATE P20 TRACK
P20 AUTO MANEUVER TO SEXTANT TRACK LM
LR - ON
POO, PITCH DOWN0.2O/SEC
ij
M S
M S
LPD ALT CE YAW RIGHT 174'
N'
N'
102:53 a
i
103:oo
:nlTlnN
Kevision
(;:c$ r \
kI
PERFORM LUNAR CHECKLIST STAY/NO STAY
DATE
I
A
SYiTEMS MONITOR
STAY/NO STAY 1 STOP 16mm CAMERA INITIATE DPS VENTING 1 ASCENT ATTE ES OFF V76 RCS MIN IMPULSE REPORT !47, !;3
I
LYIIIVI.
7.5 SEC LM ;DAI:RlBO,P286.5,YO SEC 1
PO YO
0
R 0, P -206/80, Y 0 RR TRANSPONDER - OFF V64 ACQ MSFN VHF RANGTNC m . ” , . __ _ - _ _ OFF
102:35:13
"LLAGE: 2 JET, ;; =,1;7;;NF;;
THEN 6"
,';"I:
July
TIME
8, 1969 FLIGHT
102:oo PLANNING
u
START 16mm CAMERA 3ETI:
LM CONFIRM STAY/NO STAY V44 SET LS FLAG ~&I ;M&At;/NO STAY
COPY BURN REPORT GO/NO GO
N20 AGS ALIGN CONFIGURE AGS
EVALUATE MANUAL CONTROL PITCH OVER AT P64 MANUAL ATTITUDE CONTROL TOUCHDOWN
102:46
D!JMPDSE
CSM; RO, FE+77
LPD ALTITUDE, ATTITUDE POSITION CHECK, ULLAGE 7.5 SEC
1
102:30
APOLLO 11
ANT P 220, Y 28 ACQUIRE MSFN DO1 POST BURN REPORT
LPD ALTITUDE, ATTITUDE POSITION CHECK GO/NO GO FOR PDI
102:19
:.;:;“ ,li,)‘rn ~.lAC (W)
MCC-H
LM
- 103:oo
BRANCH
1 DAY/REV 5114
STAY/NO STAY STAY/NO STAY ENABLE MSFN RELAY
PAGE 3-69
FLIGHT PLAN MCC-Ii
LM
CSM 1630 EDT
CMP
LMP
CDR
AGS LUNAR SURFACE GYRO CALIBRATION LOAD AGS ASCENT TARGET ~=6O,uuO FT, H DOT=32 Fp: CLOSE SHADES, DOFF HELMET AND GLOVES
DOFF HELMET NO5: __--.-.-N93: X
_-.-.---
Y
-
-.--
AND GLOVES
-
i M j : I N
-
2
--*--ET: ALIGN GDC. ORDEE
~57-1~~ ALIGN (REFSMMAT) 2 CELESTIAL BODIES N04: __-.-N05: __-'--
8omm/BW/CHECKLIST 60mm/HCEX/CHECKLIST
p22 AUTO MNVR TO TRACKING ATTITUDE ORB RATE(IF TIME PERMIT
N71: --)-N93 : X --.---Y 2 __.--NE9 : LAT --.--LONG/2 ALT
6 FRAMES FAR FIELD (FOCUS 50') 6 FRAMES NEAR FIELD (FOCUS 20') WITH EACH CAMERA REMOVE MAGS AND STOW INSTALL PROTECTIVE COVER AND STOW CAMERAS
- 103:39
IF NOT AT 104:lO) YO
1103:45
-REV
15
t PHOTOGRAPH'LUNAR SURFACE
GET ------INITIALIZE
1
APOLLO 11 ~I,,
;‘c,.n
1'I
"Tj
f,:r,
EDITION Revision A ,
DATE
I July
8, 1969 FLIGHT
UPLINK LGC AGS
ASCENT PAD DATA
COARSEALIGN RR CDU
TIME 103:oo
PLANNING
cAozpI~U%s
INSTALL WINDOWSHADES
I
- 104:oo
BRANCH
UPDATE CSM /
COPY P57 DATA
Lt%‘Y ANIJ LlJ&J
1 MISSION
:OPY LANDED .OCATION, GRAVITY rlEASURE
AGS LUNAR ALIGNMENT
COPY LM TRACKING PAD (SEE GET - 104:35)
RO P338/76,
~57-1~~ ALIGN (REFSMMAT) GRAVITY MEASUREMENT N04: ------
RR TO STANDBY. REPORTESTIMATE OF LANDED LOCATION CLOSE SHADES
COPY AGS AZIMUTH
DAY /REV 5114-15
& VECTOR I (TD + 1:40) UPDATE LM ( ASCENT PAD
PAGE 3-70
FLIGHT PLAN MCC-H
LM
CSM CMP S/C CONT - SCS
F
1730 EDT 104:oo
CDR
P57 - GRAVITY AND ONE CELESTIAL BODY (T-ALIGN) N04: _--.-N71: -N93: X -_.--Y --.---
/ fa
P22 AUTO MANEUVER TO TRACKING ATTITUDE? ORB RATE
LMP
REPORT:
RO, P338/342,YO
2
~ GET
-
--
-.-
---I_---
DON HELMET& GLOVES CONFIRM STAY/NO STAY
STAY/NO STAY FOR LUNAR SURFACE OPERATIONS CONFIGURE COMM DAP LOAD 12012 FOR LUNAR STAY LM WT ~.__ AGS LUNAR ALIGN
CSMWT .-~__
BIOMED SWITCH-RIGHT COPY UPDATE
P12 - ASCENTPROGRAM
V47 - INITIALIZE AGS CHECKAPS, RCS, ECS, EP AGS GUIDANCE STEERING END SIMULATED COUNTDOWNAT TIG -1 MINUTE
p&j
AGS PARTIAL POWERDOWN (AGS snvus SW -STBY) CONFIGURESYSTEMSFOR PWRDWN
CLOSEFUEL VENT
PITCH DOWNO.O5"/SEC STOP ORB RATE GO INERTIAL ROLL 170" TO ACQ MSFN V64 ACQUIRE MSFN
DOFF HELMET & GLOVES 1
I
APOLLO 11 ,u,:;(; ]~yrv. -1F
foT)
f :r
DATE
Revision \
A
July
FLIGHT
1 TIME
I 104:oo
8, 1969 PLANNING
I
EAT PERIOD (40 MIN)
L
1
EDITION
1
DOFF HELMET & GLOVES I
EAT PERIOD (40 MIN)
I MISSION
I
- 105:oo
BRANCH
STAY/NO STAY
UPDATE LM ppTi!-q 'LIFT OFF TIMES P22 AUTO OPTICS LUNAR MODULE Tll~~:~j:Q1 (HOR) T2104:39:32 __- __ __ (35") 0.2~~ ( N OR s) N89 LAT + 00.691" __ --LONG/2 t 11.858" _- --ALT - -_001.44--
(IF REQUIRED) UPLINK CMC D SIRED ORIENT m CHANGE)
I If
DAY/REV 5115
NM
PAGE 3-71
FLIGHT PLAN CSM
LM
CMP I
CDR
1830 EDT
.-
MCC-Ii LMP DUMP DSE
rP52 (OPT 1 - PREFERRED GYRO.TORQUE TO DESIRED ORIENTATION FOR PLANE CHANGE (IF PLANE CHANGE IS REOUIRED)
I
.
GDC ALIGN TO IMU F N
1 -
EAT PERIOD (40,MIN)
EAT PERIOD (40 MIN)
CONFIGURELM COMMFOR LUNAR STAY SLEEP VHF A XMIT - OFF VHF A RCV - OFF VHF B XMIT - OFF VHF B RCV - OFF
VHF AM A - SIMPLEX
,CREW STATUS REPORT (RADIATION,
:105:3D
MEDICATION)
CONFIGURE SLEEP STAYION STOW PLSS IN DONNING STATION : 105:38 EAT PERIOD (1 )UR) 1105:44 I
REV 16
REST PERIOD
REST PERIOD
(4 HPURS)
(4 HOIURS)
106:OO
MISSION APOLLO 11 ,.'k‘
EDITION
1
,,( ,‘,Y. ‘ID'1 (c)T) (?J<;\, ;
Revision \
DATE A
TIME
July 8, 1969
105:OO - 106:OO
FLIGHT
BRANCH
PLANNING
1 DAY/REV 5/15-16
PAGE 3-72
FLIGHT PLAN CSM
LM 2330 EDT llo:oo
CMP
MCC-l-l
CDR
MP
1
110:09
I i
i i i i
I 1 1 1
I
I
EAT PERIOD (1 HOUR)
IM i I4 sF ! NI I ; :I ! I
16mm/HCEX/AS PER DECAL 6Omm/FRESH HCFX/ AS 'PER DECAL“'
I-
CHANGE CO2 FILTER
110:40
PREPARATION FOR EGRESS STOW LOOSE ITEMS AND ARMREST PREPARE CAMERAS
Ir
w
j:,T;r) f;:r--
I
1
GET RCS A
B ~-
DESC A-H ASC A-H
I
I 1 lll:oo
1.1:;; -,<-,.v ,I:'/
LM CONSUMABLES UPDATE
PLSS/DPs' DONNING UNSTDW PLSS AND OPS CONFIGURE PLSS AND DPS FOR DDNNIllG
7 APOLLO 11
STAY/ND STAY
-
110:47
I
1
UPDATE LM r CAMERA EXPOSURE UPDATED FOR LM AZIMUTH AND T7 THRU T,O
STAY NO STAY FOR EVA PREP CRE,WSTATUS REPORT (SLEEP, RADIATION)
I
MISSION
DUMP DSE
1
CREW STATUS SYSTEMS PREPARATION FOR EtiRLSS -----C&W LIGHT CK, ADJUST INTERILn711 "GHTING L.
I
I
EAT PERKOD (1 HOUR) COPY 'UPDATE
?I
REST PERIOD (4 HOUR)
I
I
I I
EDITION
DATE
FINAL
JULY 1, 1969 FLIGHT
TIME llo:oo PLANNING
BRANCH
- 111:DD
DAY/REV 5/18
PAGE 3-77
FLIGHT PLAN CMP
MCC-H
LM
CSM 0030 EDT ,-111:oo
LMP
CDR
LMP UNSTOW AND DON OVERSHOES
1:
CDR UNSTOWAND DON OVERSHOES REST 'PERIOD (4 HOURS)
II iATTACH OPS TO PLSS I-
LMP DON PLSS
I: ,I-111:21
-I-
UNSTOW AND CONNECT RCU PLSS SWITCH AND VALVE POSITIONS PREPARE CDR PLSS FOR DONNING
ATTACH OPS TO PLSS CDR DON PLSS
-111:30 CO2 FILTER CHAdGE NO. 9 (11
UNSTOW AND CONNECT RCU
: 111:33
PLSS SWITCH AND VALVE POSITIONS I
INTO A, STORE 9 IN A3) I 02 FUEL CELL PURGE
1111:39 - REV 19
I EAT PERIOD (1 HOUR)
PLSSIEXTRA VEHICULAR C~MM SYSTEM ELECTRICAL CHECKOUT AUDIO SWITCHES CHECK ACTIV TE PLSS COMM SYSTEM
::::A:
(TV C4 B - CLOSE THEN OPEN 5_ r,,n Lln rnllrnUr%IT LqUlrl'ILI'II p:,:p :$z ::;:;;
UNSTOWAND CONNECT OPsx2-HOSE
-
TIME
DATE July
AND ACTUATOR
FINAL SYSTEMSPREP FOR EGRESS CONFIRM "GO" FOR CABIN DEPRESS C/B, VALVES ANU 02/H20 QUANTITY-
8,
111:oo
1969
FLIGHT
PLANNING
BRANCH
- 112:oo
DAY/REV 5118-19
GO/NO GO
PAGE 3-78
FLIGHT PLAN CSM
LM
CMP
EL/25O/BW-BRKT, (f5.6,250,INF),
CDR
INT
CHANGE SHUTTER TO l/125 PITCH UP 38" ROLL 180" TO HEADS UP RO, P320/2zg,YO PITCH DOWN, PHOTOGRAPH LM WHILE TRACKING THROUGH COAS
M S F N
STOP PITCH AND ROLL 180" TO HEADS DOWN ATTITUDE FOR SURFACE ' OBSERVATIONS STOP CAMERA
LMP
SELECT DEPLOY SITE CARRY CAMERAS DEPLOY LR3 EXPERIMENl PHOTO EXPERIMENTS
SELECT DEPLOY SITE CARRY EXPERIMENTS DEPLOY PSE TAKE CLOSEUP PHOTOS
DOCUMENTEDSAMPLE COLLECTION -___ REST/PHOTO LMP CLOSE-UP PHOTOS TETHER SAMPLE BAG TO LMP PHOTO SAMPLING UNSTOW GNOMON PHOTO DS AREA PHOTO SAMPLE COLLECTION STOW ALSCC FILM COLLECT ENVIRONMENTAL SAMPLES RETRIEVE AND STOW SWC PACK SRC CLOSE AND SEAL SRC
JOCUMENTEDSAMPLE COLLECTION MOVE BULK SRC TO STRUTS OR FOOT PAD PREPARE DS SRC
REST/PHOTOLMF
TRANSFER BULK SRC AND
\
s R180, P282/185, YO HGA P -7, Y 183
STILL CAMERA MAGAZINE REST CHECKEMU TRANSFER DS SRC I
MISSION APOLLO 11 [()T)
(.jr... :- \
COLLECT CORE TUBE SAMPLE UNSTOWTOOLS COLLECT SAMPLES STOW ALSCC FILM COLLECT ENVIRONMENTAL SAMPLES COLLECT LOOSE MATERIAL CORE TUBE SAMPLE
1+30
1t40 DUMP DSE
1+50 .M ACQUISITION ;ET:
2+00
2+10
SRC TRANSFER
)"rf,(: ),‘rr,., :I".,
MCC-!-I
,
DATE
EDITION &vision
/
A
July
TIME
8, 1969 FLIGHT
EVA TERMINATION WIPE SU T ANEFEMU WIPE FELT ON LANDING PAD AND LADDER ASCEND LADDER INGRESS CABIN CHECK LM OPERATE SEQ CAMERA RECEIVE AND STOW SRC AND MAGAZINE RECEIVE AND STOW SRC
PLANNING
114:00-115:oo BRANCH
1 DAY/REV 5/21
2+20
2t30
PAGE 3-81
FLIGHT PLAN MCC-H
LM
CSM 0430 EDT -115:oo
CMP PRESLEEP CHECKLIST CREW STATUS REPORT RADIATION, MEDICATION) CYCLE 02 & Hp FANS CHLORINATE WATER : WASTE MNGMT OVBD DRAIN VLV - OFF WASTE STOW VENT VLV CLOSED EMER CABIN PRESS VLV BOTH SURGE TANK 09 VLV - ON REPRESS PACK'02 VLV-OFF POTABLE H20 HTR - OFF SELECT COMM NORMAL LUNAR CONFIGURATION - EXCEPT: S-BAND SQUELCH ENABLE HGA TRACK - REACQ HGA BEAM - NARROW HGA P -59, Y 355 -
LMP
CDR TERMINATE EVA WIPE FEET ON LANDING PAD AND LADDER ASCEND LADDER ---I-
lr 17
CABIN REPRESS 1:
JETT EQUIP L CLOSE FWDHATCH
2+40 END EVA
POST EVA SYSTEMS CONFIGURATION CAUTION LIGHTS OFF
IT 'I
2+30
DISCONNECT RCU
115:18
DISCONNECT OPS 02 HOSES CONNECT LM 02 HOSES CONFIGURE VALVES AND CIRCUIT
BREAKERS
DISCONNECT PLSS H20 HOSES 1
SWITCH TO LM COMM SYSTEM
115:30
- 115.37 -REV
M S F N
I
PLSS/OPS DOFFING REMOVE LMP RCU OPS CHECK STOW PLSS/OPS ON CABIN FLOOR
I EAT PERIOD ('
REMOVE CDR RCU STOW PLSS/OPS ON CABIN FLOOR
6 FRAMES EACH, FAR & NEAR FIELD (FOCUS 50' & 20') AND 80mm/BW/EVA CARD iyl 6 FRAMES EACH, FAR & NEAR
nus
H"/IR)
t
;O’ &,10’)
PREP JETW -____.-FOR EQUIiMENT - .-
COPY REPORT
REPORT PLSS FEEDWATER
L
)"r:;t: Irl‘~,
]",
116:OO
MISSION
EDITION
APOLLO 11
Revisicn
(,!T)
fl!r;
:
1
REMOVE OPS,FROM PLSS
1
DATE A
July
TIME
8, 1369 FLIGHT
PLANNINS
115:00-116:00 BRANCH
DAY /REV 5/20-21
PAGE 3-82
-
UU
5, L-----
FLIGHT PLAN MCC-H
LM
CSM 1130 EDT 122:oo
CMP
LMP
CDR
LGC SELF TEST
: :
CREW STATUS REPORT (SLEEP:
i
I
:
SELECT COMM: NORMAL LUNAR CONFIGURATION CREW STATUS REPORT(SLEEP)
.
AGS TURN ON, SELF TEST AND SYSTEM TESTS INITIALIZE AGS TIME REPORT BIAS TO MCC-H REPORT: P57 - GRAVITY AND ONE CELESTIAL BODY (REFSMMAT) N04: ---.--N71: -N93: X - -f --" I
GET
?.R- ON, SELF TEST, OFF
M s L :
122:30 122:31
---.
--.---
-
T’--
--
:
AGS GYROCALIBRATE
RCS HOT FIRE
I
L
COPY TIME BIAS
M S F N
!: 122:37 V45 RESET LUNAR SURFACE FLAG
:-
P52 IMU REALIGN OPTION 3 (REFSKMAT) REPORT P52 LIFT OFF REFSMMAT
EAT PERIOD (35 MIN)
EAT PERIOD (35 MIN)
IJPL'..NK LGC ,M STATE VECTOR ISERTION +18 MIN
N71: N05: N93: X Y 123:00
Z GET: -
-
-:-
APOLLO 11 br:;L‘ F'C1‘,,..i1p 1 (f T) ji:r;r
DATE
iDlTlON
--:-
<evision
I i
‘I
I
A
July
0,
TIME 122:00
lrL9
FLIGHT
PLANNING
- 123:00
BRANCH
DAY /REV b/24
PAGE 3-88
FLIGHT PLAN MCC-H
LM
CSM 1230 EDT 123:00
CMP
LMP
CDR
UPDATE LM IASCENT PAD LCSI PAI CONSUMABLES UPDATE (A FROb! NOMINAL)
COPY ASCENT PAD LOAD PAD DATA
COPY CONSUMABLES UPDATE
AGS: AZIMUTH CORRECTION = 0 H = 60,000 FT H DOT = 32 FPS NO S-BAND YAW MNVR ORBIT INSERTION MODE
123:lO
GET: RCS TOT _ A B C
SET CAMERA FOR ASCENT 16mm/HCEX/OVERHEAD (f4,500,INF) 12 fps
I 123:24
D H2 TOT O2 TOT
RR XPONDER- SELF TEST THEN PNR
COPY CONSUMABLES UPDATE
-123:30 REV 25
02 FUEL CELL PURGE
SET UP CAMERA FOR DOCK11 16mm/l8/CEX-BRKT MIR(f8,250,INF) 6 fps
-I
REPORT: P57-GRA' VITY AND ONE Briny (T-ALIGN) CELE3TIi.bLII I__ N04: --_.N71: -N93: X _ -.-Y
__.---
z
-----
GET:
_---
LM CONSUMABLES UPDATE GET' ---I:RCS A DESC O2 DESC A-H
ASC A-H ' -:-
123:56
3 MISSION
EDITION Revision
1
APOLLO 11 by;'; ,,11^,, /]:,e
f(;;)
(:c:
124:00
;
ENTERAGS LUNAR ALIGN
+
TIME
DATE A
July
8, 1969 FLIGHT
123:00-124:00 PLANNING
BRANCH
I DUMPDSE
DAY/REV
PAGE
6124-25
3-89
FLIGHT PLAN CSM
MCC-H
LM 1330 EDT 124:OO
CMP V64 ACQUIRE MSFN VHF RANGING MNVR TO LIFT OFF RO, P250/207, YO
CDR
LMP
LOAD DAP - 12012 DON HELMET AND GLOVES L;;',;""'"' PROGRAM
DON HELMET AND GLOVES
PRELAUNCH SWITCH CK (PREI RESTRAINTS APS i
UPDATE LM p2cmm-
GO/NO GO FOR PGNCS ASCENT GUIDANCE AND LIFT OFF THIS REV PRELAUNCH SWITCH CK RESTRAINTS
LIFT OFF -6 MIN DISABLE S-BAND RELAY
LIFT OFF COMM START 16mm CAMERA
EXT RNDZ LT - ON
V47 INITIALIZE TIG-5
PITCH DOWN, O.ZO/SEC
SEC, ABORT STAGE APS, LIFT OFF
II”.
AGS
II-7.Ld.L”
BT: 7 RR LOCK ON, MODE II CONFIRM INSERTION
124:30 124:31
VHF RANGING REPORT: -~~--P52 (LIFT OFF REFSMMAT) N7,. OPTION 3 --)-.-N05: ----*--
~.-jORBIT
RR-OFF 1NSERTION VEL
124:36 124:37
ECS CHECK V48 LOAD DAP N46. 12002 V56, V41 TURN ON TRACK LIGHT
JO5: i93 :
-
-_*_
_
X
-
-.-
_
--*--__
Y
--------
;ET
---*----
--
P
-
-
_
-:-
D73 --
_
-:-
,-CT ..-a
1
APOLLO 11
(C)T) (Nov i:')
EDITION Revision A
I
DATE
I
TIME 124:OO - 125:OO
July 8, 1969 FLIGHT
A-Y ”
b
CSM: RO, P235/119, -I
125:OO
‘MISSION
DD!TWDIICT .I-.....14.
I
_
RR - ON
-----
&;I: Form ?lh'l
--_
Yo
_~ v93 (BEFORE FIRST MARK) V80, V47 INITIALIZE AGS
-..
PLANNING
BRANCH
1 DAY/REV 6125
YO
\:
IRO, P257.3,
LM FDAI:
Y
X
GET
RO, Pw/207,
P52 (LIFT OFF REFSMMAT) ,,7,: OPTION 3
/
N93:
2
INSERTION
1
PAGE 3-90
YO
FLIGHT PLAN
NOTES
EQUIPMENT STOWAGE
VACUUM PGAS
131:18
1 Ii-
131:25 REV 29
SET UP CAMERA FOR LM JETTISON 16mm/l8/CEX-BRKT,MIR (f8,750,7) 12 fps
DAP CONFIGURATION FOR LM JETTISON CSM, 0.5' DB, 0.5'/SEC A/C ROLL, 4 JET
SM RCS CHECK ENABLE JETS 8-3 AND C-4 CONFIGURE DAP - Rl=lllOZ, GO/NO-GO FOR PYRO ARM
R2=11111
GO/NO GO
i
DUMPDSE
1
!I!I
132:OO
MISSION
DATE
EDITION
1
Revision
APOLLO 11 YSC Form 29 (uay
RO, P45/25, \ HGA P-53, Y3
se)
A
July FLlOHl
I
8, 1969 PLANNINO
TIME 131:00
BUNCH
- 132:00
DAY/REV
PAGE
6129
3-97
_
MCC-n
FLIGHT PLAN
2130 EDT 132:00
NOTES’
MNVR TO TEI BURN ATTITUDE (EXCEPT ROLL) V66 - TRANS CSM STATE VECTOR TO LM SLOT BURN STATUS REPORT RECORD PRELIMINARY TE130 MNVR PAD
UPDATE piypimm
GO INERTIAL DOFF AND BAG PGA'S HELMETS AND GLOVES
1L
Y13.8 R1.l P i.2152.6 HGA P -79,Y 10
132:23
132:30
1
EAT PEI
EDITION
MISSION APOLLO 11 USC Form 29 (yay
Revision 99)
I A
ID
DATE
I
.July 8, 1969 FLlOl41
WANNINO
TIME 132:00
BRANCH
- 133:00
DAY/REV 6/29
PAGE 3-98
-
TEI BURN CHART
P OR Y RATES TEI
ATT DEVIATION
loo/SEC TAKEOVER
+10" TAKEOVER
SHUTDOWN TIME BT + 2 SEC &
AV, = -40 FPS
RESIDUALS
TRIM X AXIS TO 0.2
FPS
TEI ABORT MODES BT
TEI VGo
TRAJECTORY
ABORT MODE
I
o-01:3 0 LUNAR ORBIT MODE III
3292.7
- 1436.0
1436.0
- 1207.0
1:30-
1207.0
- Q
1:40-02:2 9 UNSTABLE/
1:4 10 UNSTABLE
MODE II
MODE
HYPERBOLIC
I
3-1 OOa
- AFTER 1 REV - 2 SPS BURNS FOR ORBIT STABILIZATION AND WATER OR CLA LANDING. I - 1 BURN AT TEI + 2 HRS P37 AT SPHERE OFINFLUENCE HYPERBOLIC (Av 580 to 0, BT ;;;;; -
Revision
A
FLIGHT PLAN 194:oo (EI -1 HR)
NOTES
PRIMARY EVAPORATOR ACTIVATION FINAL GDC DRIFT CHECK TERM CM RCS PPFHEAT SECONDARY CVAPORATOR ACTIVATION PYRO BATTEKY CHECK RECORD ENTRY PAD AND RECOVERY DATA
UPDATE p!KF
P27 UPDATE - V66 - TRANS CSM STATE VECTOR TO LM SLOT
:20 UPLINK (CSM
SET DET TO RRT EMS INITIALIZATION RSI ALIGN TO GDC CM RCS CK ENTRY BATTS - ON
194:30 (EI -30
SEPARATION CHECKLIST GO FOR PYRO ARM
GO FOR PYRO ARM
P61 ENTRY PREP MNVR TO CM/SM SEP ATT
L
ICM/SM SOP]
:5D
P62 - ENTRY ATTITUDE
1
MNVR TO ENTRY ATT
195:oo
MISSION
1
APOLLO 11 YSC Form 29 (#a~ 89)
DATE
EDITION FINAL
I
JULY 1, 1969 fLlOnT
WANNINO
TIME
I 194:oo BRANCH
- 195:oo
1 DAY/REV 9/TEC
PAGE 3-134
FLIGHT PLAN
MCC-I
P63 - ENTRY INITIATE IEI - GET = 195:05:04 1 P64 - ENTRY POST .05G
:lO TIME FROM ENTRY INTERFACE MIN:SEC
TRAJECTORY EVEN1
: 20
-
0o:oo
400,000 FEET (GET 195:05:04) ENTER S-BAND BLACKOUT 0.05G KA - INITIATE CONSTANT DRAG RDOT = -700 FPS PEAK G (6.6) SUBCIRCULAR VELOCITY P64 to P67 EXIT S-BAND BLACKOUT GUIDANCE TERMINATION DROGUE DEPLOYMENT MAIN DEPLOYMENT SPLASHDOWN
195:30
:40
L/D = 0.295,
y = -6.50",
00:18 00:28 00:52 01:18 01:22 02:08 02:OB 03:24 07:14 08:12 09:oo 13:55
V = 36,195,
& R = 1285
:50
L
196:00
MISSION APOLLO 11 YSC Form 29
DATE
EDITION (May 69)
Revision
A
July FLlOHl
8, 1969 WANNINO
TIME 195:OO - 196:00 BIAMCH
DAY /REV
PAGE
9/TEC
3-135
Related Documents 3h463d
Apollo 11 Final Flight Plan Revision A 555h15
July 2022 0
Apollo 11 1b6e4q
March 2021 0
Apollo 13 Flight Plan Final - Mar 16 1970 216e3r
December 2019 64
9 11 Plan Flight Gps 5l3w3a
October 2022 0
Saturn V Apollo Flight Configuration 1j651l
March 2023 0
Apollo 11 Mission Profile 3v2m2q
November 2019 34More Documents from "Bob Andrepont" 6e5k48
Main Engine Advanced Health Management System 6n1u44
April 2020 17
Nasa Facts International Space Station 2006 5tc1h
December 2019 44
Apollo Operations Handbook Lunar Module Lm 10 And Subsequent Vol 1 2t3a1r
August 2021 0
Apollo 11 Final Flight Plan Revision A 555h15
July 2022 0
Juno Ii Fact Sheet d396w
November 2019 57