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
in
other
is
not
working
suitable
for
general
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correspondence
DISTRIBUTION
AND RE F ERENCING
distribution
and
documents
or
referencing.
by
participating
It
may
be
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
p
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
BY
Mission
Evaluation
Team
APPROVED
BY
Manager,
George M. Low
Apollo Spacecraft
Program
NATIONAL
AERONAUTICS
MANNED
AND
SPACE
ADMINISTRATION
SPACECRAF_
CENTER
HOUSTON,
August
r
TEXAS
1969
Apollo
10
lift-off
iii
CONTENTS
Sect ion
i. 0
2.0
3.0
4.0
SUMMARY
........................
.................
..................
....
Page
i-i
2-1
3-1
4-1
4-1
4-3
.......
4-5
4-6
h-6
5-1
6-1
6-1
6-2
......
6-2
6-3
. . .
6-4
6-h
6-4
.......
6-5
6-5
6-5
6-6
7-1
7-i
7-6
7-10
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
TRANSLUNAR
INJECTION
MIDCOURSE
........
LUNAR ORBIT INSERTION
RENDEZVOUS
TRANSEARTH
TRANSEARTH
COMMAND
SERVICE
AND CIRCULARIZATION
..................
INJECTION
MIDCOURSE
ENTRY
ENTRY
.............
CORRECTIONS
.............
.............
...........
........
.......
MODULE
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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