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Engine Model: JCR. Designer: Nissan. Gross Mass: 700 kg (1,540 lb). Propellants: Solid. Diameter: 0.50 m (1.64 ft). Length: 7.00 m (22.90 ft). Country: Japan.
Engine Model: TT-500. Designer: NASDA. Gross Mass: 1,300 kg (2,800 lb). Empty Mass: 300 kg (660 lb). Propellants: Solid. Thrust(vac): 116.000 kN (26,077 lbf). Diameter: 0.50 m (1.64 ft). Length: 7.00 m (22.90 ft). Country: Japan.
Engine Model: TT-500-S2. Designer: NASDA. Gross Mass: 700 kg (1,540 lb). Empty Mass: 200 kg (440 lb). Propellants: Solid. Thrust(vac): 61.000 kN (13,713 lbf). Diameter: 0.50 m (1.64 ft). Length: 3.00 m (9.80 ft). Country: Japan.
TT-500 used on Rocket Stages - Used on stage: JCR. on launch vehicle: S.
- Used on stage: TT-500. on launch vehicle: S.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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