Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
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.

Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use