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Model: TR-1-1. Gross Mass: 10,800 kg (23,800 lb). Empty Mass: 3,900 kg (8,500 lb). Thrust (vac): 608.000 kN (136,683 lbf). Burn time: 51 sec. Propellants: Solid. Diameter: 1.10 m (3.60 ft). Length: 7.10 m (23.20 ft). Country: Japan. No Engines: 1. Motor: TR-1. Status: Retired 1998. First Flight: 1988. Last Flight: 1989. No Launched: 3. Used as: TR-1. Release conditions: NASDA.
Model: TR-1A-1. Gross Mass: 7,500 kg (16,500 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 608.000 kN (136,683 lbf). Burn time: 52 sec. Propellants: Solid. Diameter: 1.10 m (3.60 ft). Length: 7.00 m (22.90 ft). Country: Japan. No Engines: 1. Motor: TR-1. Status: Retired 1998. First Flight: 1991. Last Flight: 1998. No Launched: 7. Used as: TR-1. Other designations: TR-1A. Release conditions: NASDA.
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