spacecraft description boilerplate 13

8/3/2019 Spacecraft Description Boilerplate 13

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Access ion No. 53350-64

SM2A-O7-BP13

NASASUPPORT MANUAL

APOLLOSPACECRAFTDESCRIPTIONBOILERPLATE3

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TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 136,CONSISTING OF THE FOLLOWING:

Page No.

TitleAi thru ivI-I thru I-42-i thru Z-243-I thru 3-i04-I thru 4-285-I thru 5-66-i thru 6-47-I thru 7-248-1 thru 8-30

3

*The smetisk indicstes pages changed, added, ot deleted by the current change.

Manuals will be distributed as directed by the NASA Apollo Project Office. All requests formanuals shouldbe directed to the NASA Apollo Spacecraft Project Office at Houston, Texas.

A


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TABLE OF CONTENTS

Section

II

III

IV

Title

INTRODUCTION .........

MISSION AND OBJECTIVES ......

1-1. Purpose .........1-3 Boilerplate 13 Mission ......1-5. Apollo First Order Test Objectives1-7. Apollo Second Order Test Objectives . .

PHYSICAL DESCRIPTION .

2-1. Purpose ......2-3. Launch Escape Assembly .2- 1i. Command Module . . .2-16. Service Module and Adapter ....2-24. Interface Equipment .......2-26. Command Module to Service Module Tension Tie Bolts2-28. Umbilical Connectors . . .2-34. Launch Vehicle ....

LAUNCH ESCAPE SYSTEM .....

3-I Purpose ......3-3 Operational Description . . .3-5. Tower Jettison Motor Ignition . . .3-7. Tower Separation . . .3-9. Launch Escape Motor3-i i. Pitch Control Motor . . .3-13. Launch Escape Tower Jettison Motor .3-15. Mission Sequencer .....3-17. Tower Sequencer .....

COMMUNICATIONS AND INSTRUMENTATION

4-i4-34-4.4-Ii.

Purpose ....DescriptionCommunications EquipmentInstrumentation Equipment

Page

i

l-1

I-i1-1

i-i i-I

2-I

2-1 2-i 2-9

2-17 2 -22 2-22

2 -222 -23

3-1

3-13-i3-13-33-33-33-33-43-4

4-1

4-14-1

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SectionV

VI

VII

VIII

TitleEQUIPMENT COOLING SYSTEM ......5-i. Purpose ..................5-3. System Description ..............5-5. Principles of Operation ............ELECTRICAL POWER SYSTEM . 'i 6-1. Purpose ..................6-3. System Equipment ..............6-5. Principles of Operation ............6-9. Power Consumption .............

DOCUMENTATION AND SUPPORTING EQUIPMENT

7- i. Purpose ..................7 - 3. Documentation .............7-5. Supporting Equipment .............

ELECTRICAL SCHEMATICS ........

8- i. Purpose ........8-3. Schematic Diagrams . . .

Page

5-i

5-i5-I5-i

6-1

6-i6-i6-26-2

7-1

7-17-17-4

8-1

8-i8-1

LIST OF ILLUSTRATIONS

Figure No. Title

i-ii-2.2-i.2-2.2-3.2-42-5.2-6.2-7.2-82-9.2-I0.2-11.

Booster Compatibility Space Vehicle ..........Flight Sequence and Trajectory ...........Launch Escape Assembly .............Escape Tower Explosive Bolt ............Launch Escape Motor and Structural Skirt Area ......LES Interstage Adapter Area Components ........Nose Cone and Pitch Control Motor Area ........Command Module ................Command Module Interior .............Command Module Reference Axis ...........Dummy Shock Strut and GSE Attach Fitting .......Service Module and Adapter ............Service Module Tension Tie ............

Page

1-Z1-32-32-52-62-72-8Z-lO2-112-162-182-192 -20

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Figure3-I.3-Z.3-3.4-I.4-Z.4-3.4-4.5-1.5-Z.5-3.6-I.8-1.

8-2.

NO. Title

Launch Escape System Functional Block Diagram .....Mission Sequencer Schematic Diagram .........Tower Sequencer Schematic Diagram .........R&D Instrumentation Block Diagram .........R&D Instrumentation Locations ...........Q-Ball ...................Q-Ball Block Diagram ..............Equipment Cooling System .............Equipment Cooling System Schematic Diagram ......Equipment Cooling System Electrical Schematic ......Electrical Power System Block Diagram ........Boilerplate 13 Combined Systems Schematic

(Dwg. B14-900004, Chg. A) ...........GSE Combined Systems Schematic (Dwg. G14-900004) ....

Page

3-23-53-74-24-4

4-144-155-25-35-46-3

8-38-19

LIST OF TABLES

Table No.

2-i.2-2.2-3.3-1.3-2.

3-3.4-I.6-1.7-1.7-2.

Title

Launch Escape Assembly Physical Characteristics .....Command Module Physical Characteristics .......Command Module Compartmentation .........Time History of Events Leading to Tower Jettison .....Operational Characteristics of Launch Escape Tower

Jettison Motor ................Mission Sequencer Functions ............Measurement List ................Battery Physical Characteristics ...........Boilerplate 13 Supplementary Documents ........Ground Support Equipment .............

Page

2-12-9

2-173-i

3-43-9

4-166-17-17-4

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INTRODUCTION

This manual pertains to the mission, and provides physicaland operational descriptions of boilerplate 13, part No.BI4-00000Z-171, manufactured by Space and InformationSystems Division of North American Aviation, Inc., Downey,California. Supporting documentation and ground supportequipment is described in general terms. Functionalschematics and block diagrams are also included in thismanual. The applicability of this manual is listed in theIndex of Apollo Support Manuals and Procedures, SMIA-I.

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SECTION I

MISSION AND OBJECTIVES

I-i. PURPOSE.

l-Z, This section describes the mission and objectives of boilerplate 13 (figurel-l). A mission profile is shown in figure 1-2.

1-3. BOILERPLATE 13 MISSION.

1-4. The Apollo-Saturn compatibility tests have the initial objectives of de-veloping and qualifying the spacecraft and systems to be used for manned earth-orbital flight. The unmanned boilerplate 13 configuration is the first of theselaunch vehicle and spacecraft compatibility tests. This test will also serve todemonstrate certain environmental and systems compatibilities. Boilerplatesare research and development vehicles which simulate production spacecraft insize, shape and structural soundness. Boilerplate 13 is equipped withinstrumentation to record mission parameter data for engineering review andevaluation. The data gained from testing of boilerplate configurations will beused in determining production spacecraft flight parameters.

i-5. APOLLO FIRST ORDER TEST OBJECTIVES.

1-6. The following are the primary test objectives of the boilerplate 13 flighttest:

a. Demonstrate the physical compatibility of the launch vehicle and space-craft under preflight and flight conditions,

b. Determine the launch and exit environmental parameters for verificationof design criteria.

1-7. APOLLO SECOND ORDER TEST OBJECTIVES.

1-8. The following are the secondary test objectives of the boilerplate 13 flighttest:

a. Demonstrate the structural integrity of the launch escape system underflight loading conditions.

b. Demonstrate satisfactory launch escape tower jettison.

c. Demonstrate compatibility of the R&D communications and instrumentationsystems with launch vehicle systems.

1-1


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NORTH AMERICAN AVIATION, INC. SPACE and INFORMATION SYSTEMS DIVISI

DISTRIBUTION FOR DESCRIPTION MANUALS"(PARAGRAPH 10.3)Address

National Aeronautics and Space AdministrationAtlantic Missile Range OperationsPort Canaveral, FloridaAttn: Mr. B.P. Brown

NASA Headquarters1520 H StreetWashington, D. C.Attn: Mr. G.M. Low, MD(P)

Grumman Aircraft Engineering CorporationBethpage, Long Island, New YorkAttn: P. Gardiner

MIT Instrumentation Laboratory75 Cambridge ParkwayCambridge 39, Massachusetts

NASA Resident Apollo Spacecraft Project OfficerGrumman Aircraft Engineering CorporationBethpage, Long Island, New YorkAttn: Mr. Jack Small

National Aeronautics and Space AdministrationPost Office Drawer DWhite Sands Missile RangeWhite Sands, New Mexico

National Aeronautics and Space AdministrationManned Spacecraft CenterTransportation OfficerElington Building 381Houston, TexasAttn: Apollo Document Control CenterElington 336 - TO BE OPENED BY ADDRESSEE ONLY

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*Tile distributiol) for this report has I>eeH accomplished ill ct)mpliauce with paragraph I. 2 of Exhibit 1 contract NAS9=IS0and the Apollo Documentation Distributioil I.isI (NASA-MSC letter SP-63-478, dated2 October 1963) and revised inaccordance with NASA letter SPI-63-6:i4, dated 30 I)ut ember 19(13.


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NORTH AMERICAN AVIATION, INC.x , _./

SI A(:I : o_n(I I NI"()ItMATION SYSTEMS L)IVI_ION

Address

National Aeronautics and Space AdministrationHeadquarters NASA Plant OfficerP.O. Box 2500Daytona Beach, FloridaAttn: Administrative Contracting Officer

National Aeronautics and Space AdministrationGeorge C. Marshall Space Flight CenterHuntsville, Alabama Attn: R-SA

National Aeronautics and Space AdministrationManned Spacecraft CenterResident Apollo Spacecraft Project Office NAA12Z14 Lakewood BoulevardDowney, CaliforniaNational Aeronautics and Space AdministrationAmes Research CenterMoffett Field, California Attn: Library

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