Encyclopedia Astronautica
Northrop ALSS Rover


American manned lunar rover. Study 1964. Northrop completed Molab Studies under a Apollo Logistic Support Systems contract in March 1964.

Alternate cabin designs were considered, but all had an internal chassis and a range of 400 km with a crew of 2 on a 14 day traverse.

Variants of the standard design were:

  • M-1. Front-end airlock. Horizontal cylindrical cabin. 3010 kg, cabin volume 11.33 cubic meters.
  • M-2. Right circular cylinder, vertical cylindrical cabin. Rear end air lock. 2900 kg, cabin volume 11.33 cubic meters.
  • M-3. Horizontal cylindrical cabin. Rear end airlock. 2860 kg, cabin volume 8.5 cubic meters.
  • M-4. Horizontal truncated cylinder. Rear end airlock. 2570 kg, cabin volume 6.51 cubic meters.
  • M-5. Horizontal cylindrical cabin. Rear end airlock. 3170 kg, cabin volume 8.50 cubic meters. Considered best concept of the five.

Characteristics

Crew Size: 2.

Gross mass: 3,170 kg (6,980 lb).

More... - Chronology...


Associated Countries
See also
  • Lunar Rovers Lunar rovers were studied in a dizzying variety of sizes and shapes by NASA in the 1960's - including crawlers, trains, hoppers, and even worms. Two rovers designed for manned use actually traveled the lunar surface in the 1970's - the American two-man Lunar Rover, and the Soviet Lunokhod, which traveled the moon in robotic mode but was originally designed as emergency cosmonaut transportation. More...

Associated Manufacturers and Agencies
  • NASA American agency overseeing development of rockets and spacecraft. National Aeronautics and Space Administration, USA, USA. More...
  • Northrop American manufacturer of rockets and spacecraft. Northrop, USA. More...

Bibliography
  • Bendix Corporation, Lunar Surface Mobility Systems Comparison and Evolution Study (MOBEV), Five volumes, submitted under contract NAS8-20334, November 1966..

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