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SNA-8-D-027 (III)REV 2 CSM/LM SPACECRAFT OPERATIONAL DATA BOOK VGLIIME III MASS PROP_TIES DATA BOOK PREPARED BY SYST_L$ OPERATIONS BRANCH SYSTEMS ENGINEERING DIVISION APOLLO SPACECRAFT PROGRAM OFFICE MANNED SPACECRAFT APPROVED BY SYSTemS _INEE_ING DIVISION GEGRGE M. LOW, MANAG_ APOLLO SPACE(_RAFT PROGRAM ORFLIGHT_IONS lJ
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PRE FACE This document is the second revision issue of the Mass Properties Data Book. In this revision Missions"C", "C-Prime", "D", and "F" have been deleted. The second revision incorporates Amendments i through 65, except those amendments associated with Mis_ions "C", "C-Prime", "D", and "F". Amendments released subsequent to publi- cation of this Mass Properties Data Book, Revision 2, will be num- bered sequentially with the next revision number (i.e., 66 and on). SNA-8-D-O27(III)REV 2
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Amendment 86 9/lo/7o VOLUME IIl MASS PROPERTIES DATA BOOK 1.0 Introduction 2.0 Configuration and Reference Station Locations 3.0 Mass Properties and Loading Data by Mission 3.1 Mission G 3.2 Mission H1 3.3 Mission H2 3.4 Mission H3 3.5 Mission Jl I 4°0 CSH Reference Consumables Mass Properties Data 4.1 SPS Tank Consumables Mass Properties, Trapped Propellants, SPS Density Equations and Graphs, and SPS Loading Windows . 4.2 RCS/ECS/EPS Consumables Mass Properties 4.3 CSM RCS Load Calculatlon Tabl
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1.0 INTRODUCTION i.i SCOPE The complete Spacecraft Operational Data Book for the manned missions will consist of five separate volumes. These are defined as follows: Volume I - CSM Data Book Part I - Constraints and Performance Part II - Launch Mission Rule Redlines Volume II - LM Data Book Part I - Constraints and Performance Part II - Launch Mission Rule Redlines Volume III - Mass Properties Data Book Volume IV - EMU Data Book Volume V - ALSEP Data Book Volumes 1 and II present operational inf
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Amendment 72 10/30/69 TABLE I-I SELECTED ABBREVIATIONS AND ACRONYMS ACT Activation ACQ Acquisition ALIGN Alignment ANG Angle ASCT Ascent APS Ascent Propulsion Subsystem A/S Ascent Stage ASSY Assembly BIOINST Bioinstrumentation CAN:i Cannister CAM Camera CK Check CIRC Circularization CSC Close-Up Stereo Camera COMPT Compartment CDR Commander CM Command Module CMP Command Module Pilot CSM ConTnand Service Module COMM Communication CSI Concentric Sequence Initiation CWG Constant Wear Garment CONT C
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Anmndment 72 10130169 TABLE I-I (Continued) ICG In-FLight Coverall Garment IV I ntra vehi cul ar Jettison JETT LES Launch Escape System LEV Launch Escape Vehicle LV Launch Vehicle Left Hand LH LEB Left Hand Equipment Bay LIQ Liquid LEC Lunar Equipment Conveyor Lunar Module LM Lunar Orbit Insertion LOI Lunar Surface LS LMP LM Pilot Lunar LUN Main Chute MC Mechanism MECH Midcourse Correction MCC Not Available N/A OPS Oxygen Purge System Pair PR P-GA Pressure Garment Assembly Procedure PROC Radiati
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Amendment 72 I0/30/69 TABLE I-I (Continued) SUBSYS Subsystem SUMP Sump Tank SURF Surface SYS System RSS Root Sum Square TEMP Temporary TBD To Be Determined TEl Transearth Insertion XFR Tranfer TLI Translunar Insertion TRANS Transposi tion TRANS/DOCK Transposition and Docking UMB Umbil ical UPR Upper UEB Upper Equipment Bay UCTA Urine Collection Transfer Assembly WT Waist Tether With w/ Without w/o i-4 SNA-8-D-O27(III)REV 2
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