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Other Designations: Landing Module. Part of: Gemini Lunar Surface Rescue Spacecraft. Class: Manned. Type: Spacecraft Module. Calculated mass based on mission requirements, drawing of spacecraft, dimensions of propellant tanks. Length: 1.80 m (5.90 ft). Basic Diameter: 4.21 m (13.81 ft). Maximum Diameter: 15.00 m (49.00 ft). Mass: 20,000 kg (44,000 lb). Main Engine Thrust: 88.060 kN (19,797 lbf). Main Engine Propellants: N2O4/UDMH. Main Engine Propellants: 16,700 kg (36,800 lb). Main Engine Isp: 311 sec. Spacecraft delta v: 2,400 m/s (7,800 ft/sec). Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. | |