Table Manned Apollo Missions
Mission
Launch Date
Mission Duration
Remarks
Apollo 8
Apollo 9
Apollo 10
Apollo 11
Apollo 13
Apollo 14
Apollo 15
Apollo 16
October, 1968
December, 1968
November, 1969
May, 1969
July, 1969
Apollo 12 November, 1969
April, 1970 January, 1971
July, 1971 April, 1972
10 days, 20 hours
147 hours, 42 seconds
241 hours, 53 seconds
Apollo 17 December, 1972
192 hours, 3 minutes, 23 seconds
195 hours, 18 minutes, 35 seconds
244 hours, 36 minutes, 24 seconds
142 hours, 54 minutes, 41 seconds
216 hours, 1 minute, 58 seconds
295 hours, 11 minutes, 53 seconds
265 hours, 51 minutes, 5 seconds
301 hours, 51 minutes, 59 seconds
First manned flight test of the command service module
First manned test flight of the Apollo Saturn vehicle in lunar orbit
To test lunar landing hardware while in earth orbit
To test lunar landing hardware while in lunar orbit
To undertake the first manned lunar landing
Second lunar landing Perform surface experiments Investgigate the remains of Surveyor III
Third lunar landing aborted
Third lunar landing Perform surface experiments
Fourth lunar landing Use lunar rover vehicle
Fifth Lunar landing Exploration of the Descartes region
Sixth lunar landing Exploration of the Taurus-Littrow region
References
[1] Hallion, R., Apollo: Ten Years Since Tranquillity Base, National Air and Space Museum, Smithsonian Institution, 1979.
[2] Munford, R. and Hedrix, B., Apollo Experience Report - Command and Service Module Electrical Power Distribution Subsystem, NASA TN D-7609, March 1974.
[3] Bell III, D. and Plouche', Apollo Experience Report - Power Generation System, NASA TN D-7142, March 1973.
[4] Campos, A., Apollo Experience Report - Lunar Module Electrical Power Subsystem, NASA TN D-6977, September 1972.
[5] Trout, J., Apollo Experience Report - Battery Subsystem, NASA TN D-6976, September 1972.
[6] Apollo Spacecraft New Refemce, Space Division of North American Rockwell Corporation, December 1968.
[7] LEM Electrical Power Subsystem Study Guide, Grumman Aircraft Company, July 1966.
- FIGURE 4-1. DC Power Distribution System of the Orbiter
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