K250

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Model: Kappa 8L-1. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Burn time: 7.20 sec. Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 3.60 m (11.80 ft). Country: Japan. No Engines: 1. Motor: K250H. Status: Retired 1966. First Flight: 1960. Last Flight: 1966. No Launched: 13. Used as: K250. Release conditions: ISAS. Model: Kappa 8-2. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Thrust (vac): 34.000 kN (7,643 lbf). Burn time: 9.70 sec. Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 3.10 m (10.10 ft). Country: Japan. No Engines: 1. Motor: K250-8. Status: Retired 1970. First Flight: 1960. Last Flight: 1970. No Launched: 20. Used as: K250. Release conditions: ISAS. Model: Kappa 9M-2. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Thrust (vac): 43.000 kN (9,666 lbf). Burn time: 7.60 sec. Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 4.60 m (15.00 ft). Country: Japan. No Engines: 1. Motor: K250. Status: Retired 1988. First Flight: 1962. Last Flight: 1988. No Launched: 80. Used as: K250. Release conditions: ISAS. Used on Launch Vehicles: Kappa. 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.