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Engine Model: H-2-0. Designer: Nissan. Gross Mass: 70,400 kg (155,200 lb). Empty Mass: 11,250 kg (24,800 lb). Propellants: Solid. Thrust(vac): 1,540.000 kN (346,200 lbf). Thrust(sl): 1,336.900 kN (300,547 lbf). Isp: 273 sec. Isp (sea level): 237 sec. Burn time: 94 sec. Diameter: 1.81 m (5.93 ft). Length: 23.36 m (76.64 ft). Chambers: 1. Chamber Pressure: 46.00 bar. Area Ratio: 10.00. Country: Japan. First Flight: 1994. Last Flight: 1999. Flown: 15.

Engine Model: H-2/J-1-1. Designer: Nissan. Gross Mass: 71,100 kg (156,700 lb). Empty Mass: 11,900 kg (26,200 lb). Propellants: Solid. Thrust(vac): 1,556.600 kN (349,938 lbf). Thrust(sl): 1,414.000 kN (317,879 lbf). Isp: 273 sec. Isp (sea level): 248 sec. Burn time: 94 sec. Diameter: 1.80 m (5.90 ft). Length: 18.00 m (59.00 ft). Chambers: 1. Chamber Pressure: 58.00 bar. Area Ratio: 10.00. Country: Japan. Status: In Production.

Used in J-1-1.

H-2-0 used on Rocket Stages
  • Used on stage: H-2-0. on launch vehicle: J.
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