Corporal-1

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Model: Corporal E-1. Gross Mass: 4,500 kg (9,900 lb). Thrust (vac): 89.000 kN (20,007 lbf). Burn time: 63 sec. Propellants: Nitric acid/Aniline-Furfuyrl alcohol. Diameter: 0.76 m (2.49 ft). Length: 2.70 m (8.80 ft). Country: USA. No Engines: 1. Motor: Corporal E. Status: Retired 1951. First Flight: 1947. Last Flight: 1951. No Launched: 10. Used as: Corporal. Other designations: Corporal. Release conditions: Douglas/JPL. Model: Corporal-1. Gross Mass: 5,200 kg (11,400 lb). Thrust (vac): 89.000 kN (20,007 lbf). Burn time: 63 sec. Propellants: Nitric acid/Aniline-Furfuyrl alcohol. Diameter: 0.76 m (2.49 ft). Length: 12.00 m (39.00 ft). Country: USA. No Engines: 1. Motor: Corporal. Status: Retired 1962. First Flight: 1951. Last Flight: 1962. No Launched: 303. Used as: Corporal. Other designations: Corporal. Release conditions: Firestone. Used on Launch Vehicles: Corporal. 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.