CEV Andrews OTV

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CEV Andrews OTV

Part of Orion CEV

American manned spacecraft module. Study 2005. The Andrews CEV used a standard Orbital Transfer Vehicle for propulsion in low earth orbit or lunar transfer operations.

Status: Study 2005. Gross mass: 10,563 kg (23,287 lb). Unfuelled mass: 2,856 kg (6,296 lb). Height: 7.50 m (24.60 ft). Diameter: 4.50 m (14.70 ft).

Structure: 397 kg (875 lb). Electrical Equipment: 626 kg (1,380 lb). Miscellaneous Contingency: 623 kg (1,373 lb). RCS Propellants: 325 kg (716 lb).

Family: Manned spacecraft module. Country: USA. Spacecraft: CEV Andrews.

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