Apollo LM
Apollo LM
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Other Designations: Lunar Module. Manufacturer's Designation: LEM. Code Name: Lunar Excursion Module. Class: Manned. Type: Lunar Lander. Destination: Moon. Nation: USA. Agency: NASA. Manufacturer: Grumman.

Following the decision to use the lunar orbit rendezvous method to get to the moon, Grumman received the contract to develop the lunar module, which would take the first men to the surface to the moon. If funding had been available, modified lunar modules (dubbed LM Taxi, LM Shelter, and LM Truck) would have been used to set up the first lunar bases.

See Apollo Spacecraft Systems Development Diaries for details on development of the LM by subsystem.

Unit Cost $: 50.000 million. Crew Size: 2. Length: 6.37 m (20.89 ft). Maximum Diameter: 4.27 m (14.00 ft). Span: 9.07 m (29.75 ft). Habitable Volume: 6.65 m3. Mass: 14,696 kg (32,399 lb). Main Engine: TR-201. Main Engine Thrust: 44.041 kN (9,901 lbf). Main Engine Propellants: N2O4/Aerozine-50. Main Engine Propellants: 10,523 kg (23,199 lb). Main Engine Isp: 311 sec. Spacecraft delta v: 4,700 m/s (15,400 ft/sec). Electrical System: Batteries. Electric System: 50.00 kWh. Associated Launch Vehicle: Saturn IB, Saturn V.

  • Apollo LM ASOther Designations: Ascent Stage. Part of: Apollo LM. Class: Manned. Type: Spacecraft Module.

    Crew Size: 2. Length: 3.54 m (11.61 ft). Basic Diameter: 4.27 m (14.00 ft). Maximum Diameter: 4.27 m (14.00 ft). Habitable Volume: 6.65 m3. Mass: 4,547 kg (10,024 lb). Crew mass: 144 kg (317 lb). RCS Coarse No x Thrust: 16 x 440 N. RCS Propellants: N2O4/UDMH. RCS Isp: 290 sec. Main Engine Thrust: 15.572 kN (3,501 lbf). Main Engine Propellants: N2O4/Aerozine-50. Main Engine Propellants: 2,358 kg (5,198 lb). Main Engine Isp: 311 sec. Spacecraft delta v: 2,220 m/s (7,280 ft/sec). Electrical System: Batteries. Electric System: 17.00 kWh. Battery: 800.00 Ah.

  • Apollo LM DSOther Designations: Descent Stage. Part of: Apollo LM. Class: Manned. Type: Spacecraft Module.

    Length: 2.83 m (9.28 ft). Basic Diameter: 4.21 m (13.81 ft). Maximum Diameter: 9.37 m (30.74 ft). Mass: 10,149 kg (22,374 lb). Main Engine Thrust: 44.041 kN (9,901 lbf). Main Engine Propellants: N2O4/Aerozine-50. Main Engine Propellants: 8,165 kg (18,000 lb). Main Engine Isp: 311 sec. Spacecraft delta v: 2,470 m/s (8,100 ft/sec). Electrical System: Batteries. Electric System: 33.00 kWh. Battery: 1,600.00 Ah.


Bibliography and Further Reading
  • Loftus, J P, Journal of the British Interplanetary Society, "An Historical Overview of NASA Manned Spacecraft and their Crew Stations", 1985, Volume 38, page 354.
  • McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
  • Gatland, Kenneth, Manned Spacecraft, Macmillan, New York, 1968. ISBN: 0025428209. First of a marvelous series of pocket-size hardbacks covering spacecraft and rocketry. More at amazon.com...
  • Baker, David, The History of Manned Spaceflight, Crown, New York, 1981. The best overview of America's manned space programs up to Skylab. Information and details not available anywhere else. Unfortunately out of print and difficult to locate.
  • Furniss, Tim, Manned Spaceflight Log, Jane's, London, 1986. ISBN: 0710604025. Summary of all manned spaceflights up to 1986. Pre-Glasnost, so many 'war stories' of Soviet manned spaceflight are not included. More at amazon.com...
  • Turnill, Reginald,, The Observer's Spaceflight Directory, Frederick Warne, London, 1978. ISBN: 0723220514. Good miniature encyclopaedia of space programs just before the shuttle started flying. More at amazon.com...
  • Wade, Mark, Journal of the British Interplanetary Society, "World Manned Spacecraft Characteristics", 1981, Volume 34, page 425.
  • Kraft, Christopher C, editor, Manned Spacecraft: Engineering Design and Operation, NASA, 1968.. Collection of articles presenting technical aspects of the design of the Mercury, Gemini, and Apollo spacecraft.
  • Wilson, Keith T., Spaceflight, "EVA Log 1965-1997", 1998, Volume 40, page 85.
 
 
 
 
 
 
 
 
 

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