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Apollo command and service module

North American Aviation · Space Vehicle · United States · Early Jet (1946–1969)

Apollo command and service module — Space Vehicle
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The Apollo command and service module (CSM) was one of two principal components of the United States Apollo spacecraft, used for the Apollo program, which landed astronauts on the Moon between 1969 and 1972. The CSM functioned as a mother ship, which carried a crew of three astronauts and the second Apollo spacecraft, the Apollo Lunar Module, to lunar orbit, and brought the astronauts back to Earth. It consisted of two parts: the conical command module, a cabin that housed the crew and carried equipment needed for atmospheric reentry and splashdown; and the cylindrical service module which provided propulsion, electrical power and storage for various consumables required during a mission. An umbilical connection transferred power and consumables between the two modules. Just before reentry of the command module on the return home, the umbilical connection was severed and the service module was cast off and allowed to burn up in the atmosphere.

Specifications

Category
Space
Sub-Category
Space Vehicle
Domain
Civil
Era
Early Jet (1946–1969)
Country
United States
Manufacturer
North American Aviation
Operator
NASA
Produced
35