TT-500

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Model: TT-500-1. Gross Mass: 1,300 kg (2,800 lb). Empty Mass: 300 kg (660 lb). Thrust (vac): 116.000 kN (26,077 lbf). Propellants: Solid. Diameter: 0.50 m (1.64 ft). Length: 7.00 m (22.90 ft). Country: Japan. No Engines: 1. Motor: TT-500. Status: Retired 1983. First Flight: 1977. Last Flight: 1983. No Launched: 13. Used as: JCR. Release conditions: NASDA. Model: TT-500-2. Gross Mass: 700 kg (1,540 lb). Empty Mass: 200 kg (440 lb). Thrust (vac): 61.000 kN (13,713 lbf). Propellants: Solid. Diameter: 0.50 m (1.64 ft). Length: 3.00 m (9.80 ft). Country: Japan. No Engines: 1. Motor: TT-500-S2. Status: Retired 1983. First Flight: 1977. Last Flight: 1983. No Launched: 13. Used as: JCR. Release conditions: NASDA. Used on Launch Vehicles: S. 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.