Status: Study 1966. Thrust: 71.17 kN (15,999 lbf). Gross mass: 12,300 kg (27,100 lb). Unfuelled mass: 6,300 kg (13,800 lb). Specific impulse: 311 s. Height: 11.00 m (36.00 ft).
The basic Gemini reentry module was extended to 120 inches (3.05 m) diameter to provide a passenger compartment for up to three rescued crew. The same concept would eventually be used for Big Gemini.
Crew Size: 5. Habitable Volume: 2.55 m3. Spacecraft delta v: 2,000 m/s (6,500 ft/sec).
Family: Space station orbit. People: McDonnell. Country: USA. Launch Vehicles: Titan. Propellants: N2O4/UDMH. Agency: NASA. Bibliography: 208. Photo Gallery Gemini VariantsRetroSearch is an open source project built by @garambo | Open a GitHub Issue
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