S-250

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Model: S-250-1. Gross Mass: 200 kg (440 lb). Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 2.00 m (6.50 ft). Country: Japan. No Engines: 1. Motor: SO-250. Status: Retired 1969. First Flight: 1966. Last Flight: 1969. No Launched: 2. 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.