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Shuttle MMU

USA

Original archive entry. The text, images and links below are kept as they were written.

STS-41-B
STS-41-B
View of Astronaut Bruce McCandless during EVA
Credit: NASA

American space mobility device, tested 1984. The MMU Manned Maneuvering Unit was designed for maneuvering by astronauts untethered from the shuttle. It was used on several satellite retrieval missions in the early 1980's.

After the shuttle disaster, use of the unit was discontinued on safety grounds.

The MMU was a one-man, nitrogen-propelled backpack that latched to the Shuttle EMU spacesuit's PLSS life support system. Using rotational and translational hand controllers, the crewmember could fly with precision in or around the orbiter cargo bay or to nearby free-flying payloads or structures, and could reach many otherwise inaccessible areas outside the orbiter. Astronauts wearing MMU's deployed, serviced, repaired, and retrieved satellite payloads.

The MMU propellant - non-contaminating gaseous nitrogen stored under high pressure - could be recharged from the orbiter. The reliability of the unit was guaranteed with a dual parallel system rather than a backup redundant system. In the event of a failure in one parallel system, the system would be shut down and the remaining system would be used to return the MMU to the orbiter cargo bay. The MMU, which weighed 140 kg, included a 35-mm still photo camera that was operated by the astronaut while working in space.

Country
USA
Launch Vehicles
Space Shuttle
Agency
NASA
Bibliography
489

Chronology

2 events

1984 February 3

13:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP2. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

1984 April 6

13:58 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP1. LV Family: Shuttle. Launch Vehicle: Space Shuttle.
  • MMU 2 - . Nation: USA. Agency: NASA. Program: STS. Spacecraft: Shuttle MMU. Decay Date: 1984-04-13 . USAF Sat Cat: 14897 . COSPAR: 1984-034xx. Apogee: 496 km (308 mi). Perigee: 494 km (306 mi). Inclination: 28.50 deg. Period: 94.50 min.
  • MMU 3 - . Nation: USA. Agency: NASA. Program: STS. Spacecraft: Shuttle MMU. Decay Date: 1984-04-13 . USAF Sat Cat: 14897 . COSPAR: 1984-034xx. Apogee: 496 km (308 mi). Perigee: 494 km (306 mi). Inclination: 28.50 deg. Period: 94.50 min.