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NASA Apollo Lunar Missions



The Apollo program
included a large number of uncrewed test missions and 12 crewed missions: three
Earth orbiting missions (Apollo 7, 9 and Apollo-Soyuz), two lunar orbiting
missions (Apollo 8 and 10), a lunar swingby (Apollo 13), and six Moon landing
missions (Apollo 11, 12, 14, 15, 16, and 17). Two astronauts from each of these
six missions walked on the Moon (Neil Armstrong, Edwin Aldrin, Charles Conrad,
Alan Bean, Alan Shepard, Edgar Mitchell, David Scott, James Irwin, John Young,
Charles Duke, Gene Cernan, and Harrison Schmitt), the only humans to have set
foot on another solar system body. Total funding for the Apollo program was
approximately $20,443,600,000.

This graphic shows the
approximate locations of the Apollo moon landing sites.
Credit: NASA's Goddard Space Flight Center Scientific Visualization
Studio
NASA Apollo Lunar
Missions

The Apollo program was designed
to land humans on the Moon and bring them safely back to Earth. Six of the
missions (Apollos 11, 12, 14, 15, 16, and 17) achieved this goal. Apollos 7 and
9 were Earth orbiting missions to test the Command and Lunar Modules, and did
not return lunar data. Apollos 8 and 10 tested various components while orbiting
the Moon, and returned photography of the lunar surface. Apollo 13 did not land
on the Moon due to a malfunction, but also returned photographs. The six
missions that landed on the Moon returned a wealth of scientific data and almost
400 kilograms of lunar samples. Experiments included soil mechanics, meteoroids,
seismic, heat flow, lunar ranging, magnetic fields, and solar wind experiments.
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Did
you know that the first spacecraft to reach the Moon was in 1959?
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Did
you know that we have only sent 71 spacecraft to the Moon?
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Did
you know that only 12 people have ever set foot on the Moon?
| Pioneer
1 |
U.S.A. |
Oct
1958 |
lunar
orbit |
did
not obtain lunar trajectory, reentered on 10/12/58 |
| Pioneer
2 |
U.S.A. |
Nov
1958 |
lunar
orbit |
did
not achieve orbit |
| Pioneer
3 |
U.S.A. |
Dec
1958 |
lunar
probe |
launch
failure, reentered on 12/7/58 |
| Luna
1 |
U.S.S.R. |
Jan
1959 |
lunar
impact |
first
lunar flyby, failed to impact |
| Pioneer
4 |
U.S.A. |
Mar
1959 |
lunar
probe |
passed
within 37,300 mi. of the moon |
| Luna
2 |
U.S.S.R. |
Sept
1959 |
lunar
impact |
first
lunar impact, impacted east of the Sea of Serenity area |
| Luna
3 |
U.S.S.R. |
Oct
1959 |
lunar
probe |
first
photographs of the lunar farside |
| Pioneer
P-3 |
U.S.A. |
Nov
1959 |
lunar
orbit |
launch
failure, did not achieve orbit |
| Ranger
1 |
U.S.A. |
Aug
1961 |
lunar
probe |
launch
failure, did not escape Earth orbit, reentered on 8/30/61 |
| Ranger
2 |
U.S.A. |
Nov
1961 |
lunar
probe |
launch
failure, did not escape Earth orbit, reentered on 11/20/61 |
| Ranger
3 |
U.S.A. |
Jan
1962 |
lunar
landing |
launch
failure, missed the moon by 22,862 mi. |
| Ranger
4 |
U.S.A. |
Apr
1962 |
lunar
landing |
computer
failed, no telemetry received, crashed on the lunar farside |
| Ranger
5 |
U.S.A. |
Oct
1962 |
lunar
landing |
missed
the moon by 450 mi. |
| Sputnik
25 |
U.S.S.R. |
Jan
1963 |
lunar
probe |
unsuccessful
lunar attempt |
| Luna
4 |
U.S.S.R. |
Apr
1963 |
lunar
orbiter |
contact
lost, missed the moon |
| Ranger
6 |
U.S.A. |
Jan
/ Feb 1964 |
lunar
photography |
cameras
failed, no data returned, impacted in the Sea of Tranquillity area |
| Ranger
7 |
U.S.A. |
Jul
1964 |
lunar
photography |
transmitted
first close-up photos of the moon, impacted in the Sea of Clouds area |
| Ranger
8 |
U.S.A. |
Feb
1965 |
lunar
photography |
transmitted
high-quality photos of the moon, impacted in the Sea of Tranquillity
area |
| Ranger
9 |
U.S.A. |
Mar
1965 |
lunar
photography |
transmitted
high-quality photos of the moon, impacted in the Crater of Alphonsus |
| Luna
5 |
U.S.S.R. |
May
1965 |
lunar
lander |
first
soft-landing attempt, crashed in the Sea of Clouds area |
| Luna
6 |
U.S.S.R. |
Jun
1965 |
lunar
lander |
engine
failed, missed the moon |
| Zond
3 |
U.S.S.R. |
Jul
1965 |
lunar
probe |
photographed
lunar farside |
| Luna
7 |
U.S.S.R. |
Oct
1965 |
lunar
lander |
crashed
in the Ocean of Storms area |
| Luna
8 |
U.S.S.R. |
Dec
1965 |
lunar
lander |
crashed
in the Ocean of Storms area |
| Luna
9 |
U.S.S.R. |
Jan
/ Feb 1966 |
lunar
lander |
first
lunar soft landing, first TV transmission from lunar surface, landed on
in the Ocean of Storms area |
| Cosmos
111 |
U.S.S.R. |
Mar
1966 |
lunar
probe |
unsuccessful
lunar attempt |
| Luna
10 |
U.S.S.R. |
Mar
1966 |
lunar
orbiter |
first
lunar satellite, studied lunar surface radiation and magnetic field
intensity, monitored strength and variation of lunar gravitation |
| Surveyor
1 |
U.S.A. |
May
/ Jun 1966 |
lunar
lander |
first
soft-landed robotic laboratory, landed in the Ocean of Storms area,
returned high-quality images & selenological data |
| Lunar
Orbiter 1 |
U.S.A. |
Aug
1966 |
lunar
orbiter |
photographed
over 2 million square miles of the MoonUs surface, impacted on the lunar
far side on 10/29/66 |
| Luna
11 |
U.S.S.R. |
Aug
1966 |
lunar
orbiter |
lunar
satellite |
| Surveyor
2 |
U.S.A |
Sept
1966 |
lunar
lander |
crashed
near the Crater Copernicus |
| Luna
12 |
U.S.S.R. |
Oct
1966 |
lunar
orbiter |
lunar
satellite, transmitted large-scale pictures of the Sea of Rains and the
Crater Aristarchus, tested electric motor for lunokhod's wheels |
| Lunar
Orbiter 2 |
U.S.A. |
Nov
1966 |
lunar
orbiter |
lunar
satellite, photographed landing sites, impacted on Moon on 10/11/67 |
| Luna
13 |
U.S.S.R. |
Dec
1966 |
lunar
lander |
soft
landed in the Ocean of Storms area, measured soil density and surface
radioactivity |
| Lunar
Orbiter 3 |
U.S.A. |
Feb
1967 |
lunar
orbiter |
lunar
satellite, photographed landing sites, provided gravitational field and
lunar environment data, impacted on moon on 10/9/67 |
| Surveyor
3 |
U.S.A. |
Apr
1967 |
lunar
lander |
soft-landed
robotic laboratory, landed in the Ocean of Storms area, returned
photographs and data on a soil sample |
| Lunar
Orbiter 4 |
U.S.A. |
May
1967 |
lunar
orbiter |
lunar
satellite, provided the first pictures of the lunar south pole, impacted
on the moon on 10/6/67 |
| Surveyor
4 |
U.S.A. |
Jul
1967 |
lunar
lander |
radio
contact lost 2 1/2 min. prior to landing, impacted in Sinus Medii area |
| Explorer
35 |
U.S.A. |
Jul
1967 |
lunar
orbiter (Interplanetary Monitoring Platform 6) |
designed
to use the moon as an anchor for probing interplanetary magnetic fields,
plasma, and meteoroid fluxes |
| Lunar
Orbiter 5 |
U.S.A. |
Aug
1967 |
lunar
orbiter |
lunar
satellite, impacted on moon on 1/31/68 |
| Surveyor
5 |
U.S.A |
Sept
1967 |
lunar
lander |
soft-landed
robotic laboratory, soft-landed in the Sea of Tranquillity |
| Surveyor
6 |
U.S.A. |
Nov
1967 |
lunar
lander |
soft-landed
robotic laboratory, soft-landed in the Sinus Medii area |
| Surveyor
7 |
U.S.A. |
Jan
1968 |
lunar
lander |
soft-landed
robotic laboratory, landed near the crater Tycho |
| Luna
14 |
U.S.S.R. |
Apr
1968 |
lunar
orbiter |
lunar
satellite, studied gravitational field |
| Zond
5 |
U.S.S.R. |
Sept
1968 |
circumlunar |
first
lunar flyby and Earth return, returned to Earth on 9/21/68 |
| Zond
6 |
U.S.S.R. |
Nov
1968 |
circumlunar |
lunar
flyby and Earth return, returned to Earth on 11/17/68 |
|

|
| Apollo
8 |
U.S.A. |
Dec
1968 |
piloted
lunar orbital flight |
first
humans to orbit the moon (10 orbits) |
| Apollo
10 |
U.S.A. |
May
1969 |
piloted
lunar orbital flight |
first
docking maneuvers in lunar orbit, tested all aspects of a piloted lunar
landing |
| Luna
15 |
U.S.S.R. |
Jul
1969 |
lunar
sample return |
crashed
in the Sea of Crises area |
|

Neil
Armstrong,commander-Michael Collins,command module pilot-Edwin Aldrin,lunar
module pilot
|
| Apollo
11 |
U.S.A. |
Jul
1969 |
piloted
lunar landing |
first
humans on the moon, landed in the Sea of Tranquillity area on 7/20/69, 2
astronauts deployed experiments and collected lunar samples during lunar
EVA |
| Zond
7 |
U.S.S.R. |
Aug
1969 |
circumlunar |
lunar
flyby and Earth return, returned to Earth on 8/14/69 |
| Cosmos
300 |
U.S.S.R. |
Sept
1969 |
lunar
probe |
unsuccessful
lunar attempt, reentered 9/27/69 |
| Cosmos
305 |
U.S.S.R. |
Oct
1969 |
lunar
probe |
unsuccessful
lunar attempt, reentered 10/24/69 |
| Luna
16 |
U.S.S.R. |
Sept
1970 |
lunar
sample return |
first
robotic sample return, collected lunar samples in the Sea of Fertility
area and returned to Earth on 9/24/70 |
| Apollo
12 |
U.S.A. |
Nov
1969 |
piloted
lunar landing |
second
group of humans on the moon, landed in the Ocean of Storms area on
11/19/69, 2 astronauts deployed experi-ments, collected lunar samples,
and retrieved pieces of the Surveyor 3 spacecraft during lunar EVA |
| Apollo
13 |
U.S.A |
Apr
1970 |
piloted
lunar landing |
aborted
human landing attempt |
| Zond
8 |
U.S.S.R. |
Oct
1970 |
circumlunar |
lunar
flyby and Earth return, returned to Earth on 10/27/70 |
| Luna
17 |
U.S.S.R. |
Nov
1970 |
lunar
rover (Lunokhod 1) |
first
robotic rover, landed in the Sea of Rains area |
| Apollo
14 |
U.S.A. |
Jan
/ Feb 1971 |
piloted
lunar landing |
third
group of humans on the moon, landed in the Fra Mauro area on 2/5/71, 2
astronauts deployed experiments and collected lunar samples during lunar
EVA |
| Apollo
15 |
U.S.A. |
Jul
/ Aug 1971 |
piloted
lunar landing |
fourth
group of humans on the moon, landed in the Hadley Rille area on 7/30/71,
2 astronauts deployed experiments and collected lunar samples during
lunar EVA with lunar roving vehicle |
| Luna
18 |
U.S.S.R. |
Sept
1971 |
lunar
lander |
crashed
in the Sea of Fertility area |
| Luna
19 |
U.S.S.R. |
Sept
1971 |
lunar
orbiter |
lunar
satellite, studied moonUs gravitational field |
| Luna
20 |
U.S.S.R. |
Feb
1972 |
lunar
sample return |
second
robotic sample return, collected samples in the Sea of Crises area and
returned to Earth on 2/25/72 |
| Apollo
16 |
U.S.A. |
Apr
1972 |
piloted
lunar landing |
fifth
group of humans on the moon, landed in the Descartes area on 4/20/72, 2
astronauts deployed experiments and collected lunar samples during lunar
EVA with lunar roving vehicle |
| Apollo
17 |
U.S.A. |
Dec
1972 |
piloted
lunar landing |
sixth
group of humans on the moon, landed in the Taurus-Littrow area on
12/11/72, 2 astronauts deployed experiments and collected lunar samples
during lunar EVA with lunar roving vehicle |
| Luna
21 |
U.S.S.R. |
Jan
1973 |
lunar
rover |
robotic
lunar rover, landed near the Sea of Serenity area |
| Luna
22 |
U.S.S.R. |
May/Jun
1974 |
lunar
sample return |
lunar
satellite |
| Luna
23 |
U.S.S.R. |
Oct
1974 |
lunar
sample return |
landed
on the southern part of the Sea of Crises, sampling device
malfunctioned, no samples returned |
| Luna
24 |
U.S.S.R. |
Aug
1976 |
lunar
sample return |
third
robotic sample return, collected samples in the Sea of Crises area and
returned to Earth |
| Hiten
(Muses-A) |
Japan |
Jan
1990 |
lunar
satellite |
studied
gravity's effect on satellites, crashed on the moon on 4/11/93 |
| Clementine |
U.S.A. |
Jan
1994 |
lunar
satellite |
photographed
the lunar surface |
| Lunar
Prospector |
U.S.A. |
Jan
1998 |
lunar
polar orbiter |
determined
whether water ice exists on the Moon near its poles and mapped the
elemental composition of the lunar crust. The controlled crash of the
spacecraft into a crater on the Moon on 07/31/99 produced no observable
signature of water. |
Of the billions and billions of
people that have walked on the Earth, only a select 12 have walked on the Moon
| Neil
Armstrong |
7/20/69 |
2
hr. 31 min. 40 sec. |
| Edwin
"Buzz" Aldrin |
7/20/69 |
2
hr. 31 min. 40 sec. |
| Charles
(Pete) Conrad |
11/19/69 |
7
hr. 45 min. 18 sec. |
| Alan
Bean |
11/19/69 |
7
hr. 45 min. 18 sec. |
| Alan
Shepard |
2/5/71 |
9
hr. 22 min. 31 sec. |
| Edgar
Mitchell |
2/5/71 |
9
hr. 22 min. 31 sec. |
| James
Irwin |
7/30/71 |
18
hr. 34 min. 46 sec. |
| David
Scott |
7/30/71 |
18
hr. 34 min. 46 sec. |
| Charles
Duke |
4/21/72
to 4/23/72 |
20
hr. 14 min. 16 sec. |
| John
Young |
4/21/72
to 4/23/72 |
20
hr. 14 min. 16 sec. |
| Harrison
Schmitt |
12/11/72
to 12/13/72 |
22
hr. 3 min. 57 sec. |
| Eugene
Cernan |
12/11/72
to 12/13/72 |
22
hr. 3 min. 57 sec. |
Apollo Command
and Service Modules
The Apollo mission consisted of a Command Module (CM) and a Lunar Module (LM).
The CM and LM would separate after lunar orbit insertion. One crew member would
stay in the CM, which would orbit the Moon, while the other two astronauts would
take the LM down to the lunar surface. After exploring the surface, setting up
experiments, taking pictures, collecting rock samples, etc., the astronauts
would return to the CM for the journey back to Earth.
Spacecraft and Subsystems
As the name implies, the Command
and Service Module (CSM) was comprised of two distinct units: the Command Module
(CM), which housed the crew, spacecraft operations systems, and re-entry
equipment, and the Service Module (SM) which carried most of the consumables
(oxygen, water, helium, fuel cells, and fuel) and the main propulsion system.
The total length of the two modules attached was 11.0 meters with a maximum
diameter of 3.9 meters. Block II CSM's were used for all the crewed Apollo
missions. The Apollo 11 CSM mass of 28,801 kg was the launch mass including
propellants and expendables, of this the Command Module (CM 107) had a mass of
5557 kg and the Service Module (SM 107) 23,244 kg.
Telecommunications included
voice, television, data, and tracking and ranging subsystems for communications
between astronauts, CM, LM, and Earth. Voice contact was provided by an S-band
uplink and downlink system. Tracking was done through a unified S-band
transponder. A high gain steerable S-band antenna consisting of four 79-cm
diameter parabolic dishes was mounted on a folding boom at the aft end of the
SM. Two VHF scimitar antennas were also mounted on the SM. There was also a VHF
recovery beacon mounted in the CM. The CSM environmental control system
regulated cabin atmosphere, pressure, temperature, carbon dioxide, odors,
particles, and ventilation and controlled the temperature range of the
electronic equipment.
Command Module
The CM was a conical pressure
vessel with a maximum diameter of 3.9 m at its base and a height of 3.65 m. It
was made of an aluminum honeycomb sandwhich bonded between sheet aluminum alloy.
The base of the CM consisted of a heat shield made of brazed stainless steel
honeycomb filled with a phenolic epoxy resin as an ablative material and varied
in thickness from 1.8 to 6.9 cm. At the tip of the cone was a hatch and docking
assembly designed to mate with the lunar module. The CM was divided into three
compartments. The forward compartment in the nose of the cone held the three
25.4 m diameter main parachutes, two 5 m drogue parachutes, and pilot mortar
chutes for Earth landing. The aft compartment was situated around the base of
the CM and contained propellant tanks, reaction control engines, wiring, and
plumbing. The crew compartment comprised most of the volume of the CM,
approximately 6.17 cubic meters of space. Three astronaut couches were lined up
facing forward in the center of the compartment. A large access hatch was
situated above the center couch. A short access tunnel led to the docking hatch
in the CM nose. The crew compartment held the controls, displays, navigation
equipment and other systems used by the astronauts. The CM had five windows: one
in the access hatch, one next to each astronaut in the two outer seats, and two
forward-facing rendezvous windows. Five silver/zinc-oxide batteries provided
power after the CM and SM detached, three for re-entry and after landing and two
for vehicle separation and parachute deployment. The CM had twelve 420 N
nitrogen tetroxide/hydrazine reaction control thrusters. The CM provided the
re-entry capability at the end of the mission after separation from the Service
Module.
Service Module
The SM was a cylinder 3.9 meters
in diameter and 7.6 m long which was attached to the back of the CM. The outer
skin of the SM was formed of 2.5 cm thick aluminum honeycomb panels. The
interior was divided by milled aluminum radial beams into six sections around a
central cylinder. At the back of the SM mounted in the central cylinder was a
gimbal mounted re-startable hypergolic liquid propellant 91,000 N engine and
cone shaped engine nozzle. Attitude control was provided by four identical banks
of four 450 N reaction control thrusters each spaced 90 degrees apart around the
forward part of the SM. The six sections of the SM held three 31-cell hydrogen
oxygen fuel cells which provided 28 volts, two cryogenic oxygen and two
cryogenic hydrogen tanks, four tanks for the main propulsion engine, two for
fuel and two for oxidizer, and the subsystems the main propulsion unit. Two
helium tanks were mounted in the central cylinder. Environmental control
radiator panels were spaced around the top of the cylinder and electrical power
system radiators near the bottom.





Credit: NASA
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