CEV Andrews OTV
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
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).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- CEV Andrews