Apollo 10 Mission Report - August 1969.pdf

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AFRONAUTICS

AND

SPACE ADMINISTRATION

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APOLLO 10 MISSION REPORT

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This

only

paper

other

not

working

suitable

for

general

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correspondence

DISTRIBUTION

AND RE F ERENCING

distribution

and

documents

referencing.

participating

may

referenced

organizations.

MANNED

SPACECRAFT

HOUSTON,TEXAS

AUGUST

1969

CENTER

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APOLLO

SPACECRAFT

FLIGHT HISTORY

Mission

PA-I

Spacecraft

BP-6

Description

First pad abort

Launch date

Nov. 7, 1963

Launch site

White Sands

Missile Range,

N. Mex.

White Sands

Missile Range,

N. Mex.

Cape Kennedy 5

Fla.

Cape Kennedy,

Fla.

White Sands

Missile Range,

N. Mex.

Cape Kennedy,

Fla °

White Sands

Missile Range,

N. Mex.

Cape Kennedy,

Fla.

A-O01

BP-12

Transonic

abort

May 13, 1964

AS-101

BP-13

Nominal launch and

exit environment

Nominal launch and

exit environment

Maximum dynamic

pressure abort

May 28, 1964

AS-102

BP-15

Sept. 18, 1964

A-002

BP-23

Dec. 8, 1964

AS-I03

BP-16

Micrometeoroid

experiment

Low-altitude abort

(planned high-

altitude abort)

Micrometeoroid

experiment and

service module

RCS launch

environment

Second pad abort

Feb. 16, 1965

A-O03

BP-22

May 19, 1965

AS-104

BP-26

May 25, 1965

PA-2

BP-23A

Jane

29,

1965

White Sands

Missile Range,

N. Mex.

Cape Kennedy,

Fla.

AS-105

BP-gA

Micrometeoroid

experiment and

service module

RCS launch

environment

Power-on

boundary

tumbling

abort

July 30, 1965

A-O04

SC-002

Jan. 20, 1966

White Sands

Missile Range,

N. Mex.

Cape Kennedy,

Fla.

AS-201

SC-009

Supercireular

entry with high

heat rate

Supercircular

entry with high

heat load

(Continued

inside back

Feb. 26, 1966

AS-202

SC-011

Aug.

25, 1966

Cape Kennedy,

Fla.

cover)

_3C-00126

APOLLO

i0 MISSION

REPORT

PREPARED

Mission

Evaluation

Team

APPROVED

Manager,

George M. Low

Apollo Spacecraft

Program

NATIONAL

AERONAUTICS

MANNED

AND

SPACE

ADMINISTRATION

SPACECRAF_

CENTER

HOUSTON,

August

TEXAS

1969

Apollo

lift-off

iii

CONTENTS

Sect ion

i. 0

2.0

3.0

4.0

SUMMARY

........................

.................

..................

....

Page

i-i

2-1

3-1

4-1

4-3

.......

4-5

4-6

h-6

5-1

6-1

6-2

......

6-2

6-3

. . .

6-4

6-h

6-4

.......

6-5

6-6

7-1

7-i

7-6

7-10

7-14

INTRODUCTION

MISSION

DESCRIPTION

RENDEZVOUS

4.1

4.2

4.3

4.4

h. 5

......................

..................

.................

AND

CONTROL

TRAJECTORY

CREW PROCEDURES

GUIDANCE,

VISIBILITY

VHF RANGING

NAVIGATION,

..................

5.0

6.0

COMMUNICATIONS

TRAJECTORY

6.1

6.2

6.3

6.4

6.5

6.6

6.7

6.8

6.9

6.10

6.11

....................

......................

PHASE

PARKING

.................

ORBIT

..............

AND SEPARATION

CORRECTION

LAUNCH

EARTH

TRANSLUNAR

INJECTION

MIDCOURSE

........

LUNAR ORBIT INSERTION

RENDEZVOUS

TRANSEARTH

COMMAND

SERVICE

AND CIRCULARIZATION

..................

INJECTION

MIDCOURSE

ENTRY

.............

CORRECTIONS

.............

...........

........

.......

MODULE

LUNAR ORBIT DETERMINATION

AND SERVICE

STRUCTURAL

ELECTRICAL

CRYOGENIC

MODULE

7.0

COMMAND

7.1

7.2

7 -3

7.4

7.5

PERFORMANCE

SYST}_S

AND MECHANICAL

POWER

STORAGE

...............

...........

COMMUNICATIONS

INSTRUMENTATION

EQUIPMENT

................

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