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
Gemini AM
Part of Gemini Family
American manned spacecraft module. 12 launches, 1964.04.08 (Gemini 1) to 1966.11.11 (Gemini 12).

AKA: Adapter Module. Status: Operational 1964. Gross mass: 591 kg (1,302 lb). Unfuelled mass: 491 kg (1,082 lb). Specific impulse: 255 s. Height: 0.92 m (3.01 ft). Diameter: 2.59 m (8.49 ft).

Structure: 160 kg (350 lb). Reaction Control System: 200 kg (440 lb). RCS Coarse No x Thrust: 6 x 420 N. RCS specific impulse: 273 sec. Spacecraft delta v: 101 m/s (331 ft/sec).



Family: Manned spacecraft module. Country: USA. Spacecraft: Gemini. Propellants: Solid.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use