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PAYLOADS ARE IN RED
APOLLO
CREWS
www.apogeebooks.com
BOOST
PROTECTIVE
COVER
LAUNCH
ESCAPE
SYSTEM
APOLLO 1
VIRGIL GRISSOM
ROGER CHAFFEE
EDWARD WHITE
COMMAND
MODULE
SERVICE
MODULE
APOLLO
SERVICE
MODULE
ENGINE
APOLLO 7
WALLY SCHIRRA
WALTER CUNNINGHAM
DONN EISELE
LUNAR
MODULE
SPACECRAFT
LM
ADAPTER
SA-1
10/27/61
Dummy
R&D, test S-1
stage propulsion, verify
structure and
dynamics
1st flight of
Saturn
Rocket.
Suborbital
flight 52,500
kg to 136km
SA-2
SA-3
4/25/62
11/16/62
95 tons of
95 tons of
water (Project water (Project
Highwater).
Highwater).
R&D,Water R&D, observe
dispersion at water disperhigh altitude.
sion at high
Self destruct
altitude
activated at 167km. 1st full
105 km. Ice
propellant
cloud 56km
load. 1st test
high was
of Block II
formed. New
anti-sloshing stage separa-
baffles used
tion retros.
SA-4
3/28/63
Dummy
LJ-11-QTV
8/28/63
Dummy
LESPA-1
11/7/63
BP-6
SA-5
1/29/64
Dummy
LJ-11-A-001
5/13/64
BP-12
SA-6
5/28/64
BP-13
R&D, demo
engine-out
capability. #5
Engine shut
off at T+ 100
seconds.
Aerodynamic
tests using
dummy Block
II fairings.
Apogee
129km
Little Joe
launch vehicle
demonstration
test Algol
motor termination test.
Destruct system malfunctioned.
Total weight
25,984kg.
Apogee 5.6km
Boilerplate
Apollo spacecraft.Test the
LES ability to
work in emergency before
launch while
on the pad.
Total weight
9800kg
Apogee
2.8 km
1st S-IV flight
1st Block II
booster. 1st
use of six RL10 hydrogen
engines on
2nd stage.
16,965 kg in
orbit, the
heaviest payload to that
date.
LES integrity
and efficacy
test, command
module/
service
module separation test.
Aerodynamic
load test.
Total weight
26,139kg
Apogee 5.9km
Boilerplate
Apollo
spacecraft.
One inboard
engine unexpectedly shut
down 26 sec.
early but did
not impair
flight. 17650kg
to orbit of
approx.200km
SA-7
9/18/64
BP-15
LJ-11-A-002
12/8/64
BP-23
SA-9
2/16/65
BP-16
Pegasus 1
Boilerplate
Apollo
command
module. 1st
operational
flight. Pegasus
1 satellite
inside dummy
Service
Module placed
into approx.
500km orbit.
Boilerplate
Test LES at
Apollo space- Max Q.Test
craft. 39,000 CM pressure
lbs into orbit. loads, canard
Declared
deployment,
operational
BPC separathree flights
tion, chutes
early. 16700kg and landing
to orbit of
system.
approx.
Total weight
200km.
42,288kg
Apogee 5km
LJ-11-A-003
5/19/65
BP-22
Test escape
system at
upper altitude
for canards,
heat shield
orientation,
BPC jettison,
window
degradation,
thermal
effects.
Total weight
80,372kg
Apogee 6km
APOLLO 8
FRANK BORMAN
WILLIAM ANDERS
JAMES LOVELL
HYDROGEN
VENT
S-IVB
FORWARD
SKIRT
STRUCTURE
CABLE
TUNNEL
COLD
HELIUM
SPHERES (8)
AUXILIARY
PROPULSION
SYSTEM
MODULE
LIQUID
HYDROGEN
TANK
APOLLO 9
JAMES MCDIVITT
RUSSELL SCHWEICKART
DAVID SCOTT
LIQUID
OXYGEN
TANK
THRUST
STRUCTURE
ULLAGE
MOTORS (2)
AMBIENT
HELIUM
REPRESSURIZATION
SPHERES (10)
J-2
ENGINE
APOLLO 10
THOMAS STAFFORD
EUGENE CERNAN
JOHN YOUNG
AFT
INTERSTAGE
STRUCTURE
RETRO
MOTORS (4)
APOLLO 11
NEIL ARMSTRONG
BUZZ ALDRIN
MICHAEL COLLINS
ACRONYMS:
ALSEP - Apollo Lunar Surface
Experiments Package
AS - Apollo/Saturn
ATM - Apollo Telescope Mount
BP - Boilerplate Spacecraft
BPC - Boost Protective Cover
CM - Command Module
CSM - Command Service Module
EASEP - Early Apollo Surface
Experiments Package
EREP - Earth Resource
Experiment Package
EVA - Extravehicular Activity
LES - Launch Escape System
LH2 - Liquid Hydrogen
LJ - Little Joe Booster
LM - Lunar Module
LRV - Lunar Roving Vehicle
LTA - Lunar Test Article
O2 - Oxygen
SA - Saturn booster
SLA - Spacecraft LM Adapter
SM - Service Module
S-II
APOLLO 12
CHARLES CONRAD
ALAN BEAN
RICHARD GORDON
FORWARD
SKIRT
FUEL TANK
(LH2)
APOLLO 13
JAMES LOVELL
FRED HAISE
JOHN SWIGERT
TUNNEL
SA-8
5/25/65
BP-26
Pegasus 2
Boilerplate
Apollo command module.
Pegasus 2
satellite
launched
inside dummy
Service
Module placed
into approx.
600km orbit.
LESPA-2
6/29/65
BP-23A
Test the LES
ability to work
on pad with
full BPC,
canards, jettisonable apex
and dual
reefed drogue
chutes.
Total weight
9800kg
Apogee 2.8km
SA-10
7/30/65
BP-9
Pegasus 3
Boilerplate
Apollo command module.
Pegasus 3
satellite
launched
inside dummy
Service
Module placed
into approx.
550km orbit.
LJ-11-A-004
1/20/66
CM002
Test Launch
escape system
in power on
tumbling
abort, canard
orientation
ability, loads
on CM,
window
degradation.
Total weight
63,381kg
Apogee
23.8km
AS-201
2/26/66
CSM-009
AS-203
7/5/66
LH2 in S-IVB
AS-202
8/25/66
CSM-011
Launch vehicle
Launch vehicle
Launch vehicle
and CSM
and CSM
development. development. development.
Demo of
Test of CSM
Test of CSM subcontrol of
subsystems and
systems and of
LH2 by
structural
the spare vehicle.
continuous integrity. Demo
Demonstration
venting in
of propulsion
of reentry
adequacy of the orbit. 1st flight and entry conof Saturn
trol by G&N
CM at earth
Instrument
system.
orbital
Unit. 212km
Re-entry at
conditions.
apogee.
28,500 fps.
500km apogee
APOLLO 4
(SA-501)
11/9/67
CSM-017
LTA-10R
1st Saturn V
flight.
Launch vehicle
and spacecraft
development.
Demonstration
of Saturn V
performance
and of CM
entry at lunar
return velocity.
APOLLO 5
(SA-204)
1/22/68
LM-1
SLA-7
LM development.Verified
operation of
ascent and
descent
propulsion and
structures.
Evaluation of
LM staging and
S-IVB/IU orbital
performance.
APOLLO 6
(SA-502)
4/4/68
CM-020
SM-014
LTA-2R
2nd Saturn V
flight.
Launch vehicle
and spacecraft
development.
Demonstrate
Saturn V
Launch Vehicle
performance.
APOLLO 7
(SA-205)
10/11/68
CM-101
SM-101
APOLLO 8
(SA-503)
12/21/68
CM-103
SM-103
LTA-B
Manned CSM
operations.
1st manned
Apollo
flight.1st lunar
duration mission. 14,781kg
in orbit.
Duration 10
days 20 hours.
OXIDIZER
TANK
(LOX)
AFT
SKIRT
APOLLO 9
(SA-504)
3/3/69
CM-104
SM-104
LM-3
APOLLO 14
ALAN SHEPARD
EDGAR MITCHELL
STUART ROOSA
J-2 ENGINE
(5)
1st cislunar
Earth orbital
manned flight. mission. 1st
Lunar orbital joint manned
mission.Ten
SM/LM
lunar orbits.
operations.
Mission
1st manned
duration 6
LM flight.
days 3 hours. Duration 10
days 1 hour.
APOLLO 15
DAVID SCOTT
JAMES IRWIN
ALFRED WORDEN
AFT
INTERSTAGE
8 ULLAGE ROCKETS
22,900 LB THRUST
EACH
APOLLO 16
JOHN YOUNG
CHARLES DUKE
THOMAS MATTINGLY
OXIDIZER
VENT
S-IC
FORWARD
SKIRT
STRUCTURE
APOLLO 17
EUGENE CERNAN
HARRISON SCHMITT
RON EVANS
OXIDIZER
TANK
(LOX)
HELIUM
BOTTLES (4)
APOLLO/ SATURN-V MAXIMUMS
(APOLLO 17)
LAUNCH WEIGHT - 6,445,000 POUNDS
TO LEO - 311,000 POUNDS
TO LUNAR ORBIT - 76,000 POUNDS
SKYLAB 2
CHARLES CONRAD
PAUL WEITZ
JOE KERWIN
CRUCIFORM
BAFFLES
SKYLAB 3
ALAN BEAN
OWEN GARRIOTT
JACK LOUSMA
OXYGEN
SUCTION
LINES
FUEL TANK
(RP-1)
SKYLAB 4
GERALD CARR
ED GIBSON
WILLIAM POGUE
FIN
APOLLO 10 APOLLO 11
(SA-505)
(SA-506)
7/16/69
5/18/69
CM-107
CM-106
SM-107
SM-106
LM-5
LM-4
SLA-14
EASEP
Lunar orbital
1st manned
mission.
lunar landing
Evaluate LM
mission.
performance in
cislunar environ- Deploy EASEP.
Lunar surface
ment, following stay time 21.6
lunar landing hours. Mission
profile. Mission
duration 8
duration 8 days. days 3 hours.
APOLLO 12
(SA-507)
11/14/69
CM-108
SM-108
LM-6
SLA-15
ALSEP
2nd lunar
landing. Point
landing, deploy
ALSEP, investigate Surveyor
III Lunar surface stay time
31.5 hours.
Mission
duration 10
days 4.6 hrs.
APOLLO 13 APOLLO 14 APOLLO 15
(SA-508)
(SA-509)
(SA-510)
4/11/70
1/31/71
7/26/71
CM-109
CM-110
CM-112
SM-109
SM-110
SM-112
LM-7
LM-8
LM-10
SLA-16
SLA-17
SLA-19
ALSEP
ALSEP
ALSEP
LRV-1
Planned 3rd
3rd lunar
4th lunar landlunar landing. landing. Fra
ing Hadley
Aborted at
Mauro site. site.Traverses
approx. 56 hrs Deploy ALSEP. in 1st LRV
due to loss of Geology tra- deploy ALSEP.
cryogenic O2 verse. Lunar
Lunar stay
and loss of stay time 34.5 time 66.9 hrs.
electrical
hours. Mission
Mission
power and
duration 9
duration 12
water.
days 2 min.
days 7.2 hrs.
APOLLO 16
(SA-511)
4/16/72
CM-113
SM-113
LM-11
SLA-20
ALSEP
LRV-2
5th lunar landing Descartes
site. Deploy
ALSEP.Three
EVAs in LRV.
Lunar stay
time 71 hours.
Mission
duration 11
days 1.8 hrs.
APOLLO 17
(SA-512)
12/7/72
CM-114
SM-114
LM-12
SLA-21
ALSEP
LRV-3
6th lunar landing TaurusLittrow site.
Deploy ALSEP
3 EVA's in
LRV Lunar
stay time 75
hrs. Mission
duration 12
days 14 hrs.
SKYLAB 1 SKYLAB 2 SKYLAB 3
(SA-513)
(SA-206)
(SA-207)
5/14/73
5/25/73
7/23/73
Multidocking
CSM-116
CSM-117
adapter, ATM
Workshop,
1st manned
2nd manned
Airlock.
launch to
launch to
Launch placed Skylab space Skylab space
Skylab
station.
station. Solar
workshop Repaired dam- data, EREP, &
space station
aged solar
biomedical
in 433km
array and
experiments.
circular orbit.
deployed
Duration
Solar panels
parasol.
59 days
damaged on
Duration
launch.
28 days
SKYLAB 4
(SA-208)
11/16/73
CSM-118
ASTP
(SA-210)
7/15/75
CSM-111
Docking
3rd manned
Adapter
launch to
Conduct
Skylab space
manned
station. Solar rendezvous &
data, EREP, & docking with
biomedical
USSR Soyuz.
experiments.
Duration 9
Duration
days 1 hr
84 days
(Apollo) 5
days 22 hrs
(Soyuz)
APOLLO-SOYUZ
THOMAS STAFFORD
DEKE SLAYTON
VANCE BRAND
ENGINE
FAIRING
F-1
ENGINE (5)
©2006 Apogee Books, Box 62034, Burlington, Ontario, L7S1W3, Canada www.apogeebooks.com