CEV Andrews MM

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CEV Andrews MM

Part of Orion CEV

American manned spacecraft module. Study 2005. The Andrews CEV mission module provided a pressurized cabin for use by the crew while in transit from the moon to the earth.

Status: Study 2005. Gross mass: 1,328 kg (2,927 lb). Height: 3.70 m (12.10 ft). Diameter: 2.70 m (8.80 ft).

Development Cost $: 158.000 million. Unit Cost $: 37.000 million. Cost Notes: First unit cost; 2005$; ops cost $14.5 million/mission.. Structure: 943 kg (2,078 lb). Heat shield: 98 kg (216 lb). Miscellaneous Contingency: 221 kg (487 lb).

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

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