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Apollo 11 Mission Report PDF

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=-·. MSC-00171 NATIONALA ERONAUTICASN D SPACEA DMINISATTRION APOLL1O1 M ISOS[ORNE PROT I \ \ :Jj MANNED SPACECRAFCTE NTER HOUSTON,TEXAS NOVEMBE1R9 69 APOLLSOP ACECRAFFTL IGHHTI STORY Mission S12acecraft Description Launcdha te Launchs ite PA-l BP-6 Firstp ada bort Nov.7 , 1963 WhiteS ands MissilRean ge, N.M ex. A-001 BP-12 Transonaibco rt Ma;y 13,1 964 White Sands MissilRea nge, N.Me x. � 1- AS-101 BP-13 Nominalla uncahn d Ma;y2 8,1 964 CapeK ennedy, exite nvironment Fla. . - !' AS-102 BP-15 Nominalla uncanhd Sept.1 8,1 964 CapeK ennedy, exite nvironment Fla. A-002 BP-23 MaximUIIl dynamic Dec.8 , 1964 WhiteS ands pressuraeb ort MissilRea nge, --� \.__.- ::_, N. Mex. AS-103 BP-16 Micrometeoroid Feb.1 6,1 965 Cape Kennedy, experiment Fla. A-003 BP-22 Low-altituadbeo rt Ma;y 19,1 965 White Sands (plannheidgh - MissilRea nge, altitudaeb ort) N. Mex. AS-104 BP-26 Micrometeoroid Ma;y 25, 1965 CapeK ennedy, ..;;__ experimenantd Fla• servicmeo dule RCSl aunch environment PA-2 BP-23A Seconpda da bort June 29,1 965 WhiteS ands MissilRea nge, N.Mex. AS-105 BP-9A Micrmoeteoroid July3 0,1 965 CapeK ennedy, experimeanntd Fla. servicmeo dule RCSl aunch environment -, A-004 SC-002 Power-otnum bling Jan. 20,1 966 WhiteS ands boundarayb ort MissilRea nge, N.M ex. AS-201 SC-009 Supercircular Feb.2 6,1 966 CapeK ennedy, entryw ithh igh Fla. heatr ate \ AS-202 SC-Oll Supercircular Aug.2 5,1 966 CapeK ennedy, entryw ithh igh Fla. heat load (Continuiends idbea ck cover) MSC-00171 APOLL1O1MI SSIORNE PORT PREPARBEYD Missin oEvaluiaont Team / APPROVBEYD c� Geo�r gMe.L L.c.r- o-w Manaegr,A pollSop acefctrP arogram NATNIOALA ERONAUTIACNSDS PACAED MINISATTRION MANNEDS PACECRCAENFTT ER HOUST,OT NEXAS Novemb1e96r9 ----·- --·--___...- --.,__ "Huostotnh,eE aghlaesl anded." iii CONTENTS Section Page 1.0 SUMMARY 1-1 2.0 INTRODUCTION 2-1 3.0M ISSIODNE SCRIPTION 3-1 4.0 PILOTSR'E PORT 4-1 4.1 PRELAUNACCTHI VITIES 4-1 4.2 LAUNCH 4-1 4.3 EARTHO RBITC OASTA NDT RANSLUNIANRJ ECTION 4-1 / 4.4 TRANSPOSITAINODND OCKING 4-2 4.5 'TRANSLUCNOAARS T 4-2 4.6 LUNARO RBITI NSERTION 4-3 4.7 LUNARM ODULEC HECKOUT 4-4 4.8 DESCENPTR EPARATI.O N 4-4 4.9 UNDOCKIANNGD S EPARATION 4-7 4.01 LUNARM ODULDEE SCENT 4-7 4.11 COMMAND MODULSEO LOA CTIVITIES 4-9 4.21 LUNARS URFACOEP ERATIONS 4-10 4.31 LAUNCPHR EPARATION 4-16 4.41 ASCENT 4-17 4.15 RENDEZVOUS 4-17 4.61 COMMAND MODULED OCKING 4-18 .#- 4.71 TRANSEARTIHN JECTION 4-19 r 4.81 TRANESA RTHC OAST 4-19 -'" •1 4.91 ENTRY. 4-20 ......."' 4.02 RECOVERY 4-20 5.0L UNRA DESCENATN DA SCENT 5-1 5.1 DESCENTTR AJECTOLROYG IC 5-1 5.2 PREPARATIFOONR P OWEREDDE SCEN1� 5-2 5.3 POWEREDDE SCEN.T . 5-4 iv Sectni o Page 5.4 LADNIGN DYNAMIC.S . 5-6 5.5 POSATNLDIGN SPACCREAFTO PERATIONS 5-7 5.6 ASCENT 5-8 5.7 RENDEZVOUS 5-10 6.0 COMMUNICIAOTNS 6-1 -� -----. 7.0 TRAJECTORY 7-1 7.1 LANUCHP HASE 7-1 "'-- 7.2 EARTPHARK INGO RBIT 7-1 7.3 TRANSLUNIANRJ ECTION 7-1 (o- 7.4 MANEUVERA LYSIS. 7-2 AN 7.5 COMMANDM ODULEEN TRY 7-4 7.6 SEVRICEM ODULEEN TRY 7-5 7.7 LUNAORR BITTA RGEGT IN 7-5 7.8 LUNAORR BINTA VIGIAOTN . 7-6 8.0 COMMANDA NDS EVRICME ODULPEE RFORMANCE 8-1 8.1 STRCUTURAALN DME CHANICSAYLS TEMS 8-1 8.2 ELECTRIPCOAWLE R 8-4 8.3 CRYOGESNTIOCAR GE 8-5 8.4 VHFR ANGI.N G 8-5 8.5 INSRTUMENTATION 8-5 8.6 GUIDCAEN,N AVIGIAOTN,A NDC ONTROL 8-6 8.7 REACTICOONN TROL 8-19 8.8 SERVIPCREO PULSION 8-19 8.9 ENVIRONMENCTOANLT RSOYLS TEM 8-23 ·-. 8.01 CRESWT ATION 8-24 8.11 CONMSAUBLES 8-25 9.0 LUNAMRO DULPEE RFMOARCNE 9-1 9.1 STRUCRTAULA NDME CHANICSAYLS TEMS 9-1 9.2 THERMCAOLN TR.O L 9-1 9.3 ELECTRICPAOLW ER 9-2 v Section Page 9.4 COMMUNICATIONESQ UIPMENT 9-2 9·5 INSTRUMENTATION 9-3 96. GUIDANCAEN DC ONTROL 9-3 97. REACTIONC ONTRLO 9-19 9.8 DESCENPTR OPULSION 9-22 9·9 ASCENPTR OPUSLION. 9-27 9.01 ENVIRONMENTCAOLN TROSLY SETM 9-29 9.11 RADAR. . . 9-29 91.2 CREWS TATION 9-30 91.3 CONSUMABLES 9-30 10.0 EXTRAHVIECULAMRO BILITUYN ITP ERFORMANCE 10-1 11.0 THEL UNARS URFAC.E . . 11-1 11.1 LUNARG EOLOGEYXP ERIMENT 11-3 11.2 LUNARS URFACMEEC HANICESXP ERIMENT 11-12 11.3 EXAMINATIONO F LUNARS AMPLES 11-14 n.4 PASSIVSEE ISMICE XPERIMENT 11-17 11.5 LASER RANGINRGE TRQ-REFLECETXPOERR IMENT 11-22 11.6 SOLARW INDC OMPOSITIOENXP ERIMENT 11-23 11.7 PHOTOGRAP.H Y 11-23 12.0 BIOMEDICAELV ALAUTION 12-1 12.1 BIOINTSRUMENTATIOANN DP HYSIOLOGIDCAATLA 12-1 12.2 MEDICALO BSERVATIONS 12-2 12.3 EXTRAVEHICUALCTAIRV ITY 12-5 12.4 PHYSICA�XLAMI NATIONS 12-5 12.5 LUNAR CONTAMINATIAONND Q UARAN'nNE 12-6 -. 13.0 MISSIOSNU PPORPTE RFORMANCE 13-1 13.1 FLIGHCTO NTROL 13-1 13.2 NETWORKP ERFORMANCE 13-2 13.3 RECOVERY OPERATIONS 13-3 vi Section Page 14.0 ASSESSMEONFTMI SSIOONB JECTIVES 14-1 14.1 LOCATIOOFNL ANDELDU NAMRO DULE 14-1 14.2 LUNAFRI ELGDE OLOGY 14-2 15.0 LAUNCH VESHUMIMARCLEY 15-1 16.0 ANOMASLY RY. 16-1 UMMA 16.1 COMMAN D ANDS ERVIMCOED ULES 16-1 16.2 LUNAMRO DULE 16-9 16.3 GOVERNMENT-FURENQIUSIHPEMEDN T 16-21 17.0 CONCLUSI.O NS 17-1 APPENDAI X-V EHICDLEES CRIPTIONS A-1 A.1 COMMANDA NDS ERVIMCOED ULES A-1 A.2 LUNAMRO DULE . . A-1 A.3 EXTRAVEHICMUOLBAIRL IUTNYI T A-5 A.4 EXPERIMENETQ UIPMENT A-8 A.5 LAUNCVHE HICLE A-10 A.6 MASSP ROPERTIES A-10 APPENDBI X-S PACEC HISTORIES B-1 RAFT APPENDCI X-P OSTFLITGEHSTT ING C-1 APPENDDI X-D ATAA VAILABILITY D-1 APPENDEI X-G LOSSARY E-1 vii SYMBOLASN DA BBREVIATIONS A ampere ac alternatciunrgr ent AGS aborgtu idanscyes tem A-h ampere-hour ALDS Apollloa uncdha tasy stem arcs ec arcs econd -� ARIA Apollroan gei nstrumentaatiirocnr aft BDA Bermuda Btu Brtiisht hermal unit CAPC OM capsucloem municator CATS commanandd telemetsryys tem c.d.t. central daylight time em centimeter CMC commamnodd ulceo mputer CRO CarnarvoAnu,s rtalia ·csM commanandd servimcoed ules CYI CanaryI slands D down decibe(la lsuos edas dBm) dB de direcctu rrent deg degree D/T delayteidm e E east e.s.t. eastesrnt andatridm e FM frequenmcoyd ulation - f't/sec feetp ers econd g graviotfye arth G&N guindcaean d navigiaotn GDS Goldosnte,C alifornia G.mt.. Greenwimceha nt ime viii HAW Hawaii hr hour HSK HoneysuckAlues,t ralia Hz hertz I inertia in-lb inch-pound kpps kilopulspeesr s econd kW-h kilowattu-rh o lb/hr poundsp erh our lb/ft2 poundpse rs quarfeo ot LGC lunar modulgeu idaen ccomputer lunar module LM M mega- MAD Madrid,S pain mERU milli-eahr rtateun it mg milligram MILA MerritIts lanLda unch AreFal,o rida min minute millimeter msec millisecond mm MSFN ManneSdp aceF lighNte twork N north NA nota vailable pressurter ansducleorc ation p ( ) PAM pulseam plitudmeo dulation PCM pulsec odem odulation PM phasem odulation ppm partsp erm illion psf poundpse rs quarfeo ot psi poundpse rs quarien ch q dynamipcr essure RED Redstonter ackinsgh ip

Description:
ampere alternating current abort guidance system ampere-hour. Apollo launch data system arc second. Apollo range instrumentation aircraft.
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