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User:JustinTime55/sandbox/Apollo CSM infobox

From Wikipedia, the free encyclopedia
Apollo Command/Service Module
Apollo 15 Command and Service Module in lunar orbit
ManufacturerNorth American Aviation
North American Rockwell
DesignerMaxime Faget
Country of originUnited States
OperatorNASA
ApplicationsManned lunar landing
Skylab crew shuttle
Apollo-Soyuz Test Project
Specifications
Launch mass32,390 pounds (14,690 kg) Earth orbit
63,500 pounds (28,800 kg) Lunar
Dry mass26,300 pounds (11,900 kg)
Payload capacity2,320 pounds (1,050 kg)
Crew capacity3
Dimensions36.2 feet (11.0 m) high
12.8 feet (3.9 m) diameter
Volume218 cubic feet (6.2 m3)
PowerFuel cells
RegimeLow Earth orbit
Cislunar space
Lunar orbit
Design life14 days
Production
StatusRetired
Built35
Launched19
Operational19
Failed2
Lost1
Maiden launchFebruary 26, 1966
Last launchJuly 15, 1975
Last retirementJuly 24, 1975

Configuration

Apollo Block II CSM diagram
← Gemini spacecraft