TR-1

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Engine Model: TR-1. Designer: NASDA. Gross Mass: 10,800 kg (23,800 lb). Empty Mass: 3,900 kg (8,500 lb). Propellants: Solid. Thrust(vac): 608.000 kN (136,683 lbf). Burn time: 51 sec. Diameter: 1.10 m (3.60 ft). Length: 7.10 m (23.20 ft). Country: Japan. TR-1 used on Rocket Stages Used on stage: TR-1. on launch vehicle: TR-1. 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.