| Rescue Gemini | ||
A version of Gemini was proposed for rescue of crews stranded in Earth orbit. This version, launched by a Titan 3C, used a transtage for maneuvering. 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. Length: 11.00 m (36.00 ft). Maximum Diameter: 3.05 m (10.00 ft). Habitable Volume: 2.55 m3. Mass: 12,300 kg (27,100 lb). Main Engine Thrust: 71.166 kN (15,999 lbf). Main Engine Propellants: N2O4/UDMH. Main Engine Propellants: 6,000 kg (13,200 lb). Main Engine Isp: 311 sec. Spacecraft delta v: 2,000 m/s (6,500 ft/sec). Electrical System: Fuel cells. Associated Launch Vehicle: Titan 3C. Bibliography and Further Reading
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