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H-2/J-1-1
Part of H-2-0 Family
Nissan solid rocket engine. In Production. Used in J-1-1.

Status: In Production. Thrust: 1,556.60 kN (349,938 lbf). Gross mass: 71,100 kg (156,700 lb). Unfuelled mass: 11,900 kg (26,200 lb). Specific impulse: 273 s. Specific impulse sea level: 248 s. Burn time: 94 s. Height: 18.00 m (59.00 ft). Diameter: 1.80 m (5.90 ft).

Thrust (sl): 1,414.000 kN (317,879 lbf). Thrust (sl): 144,194 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 10.



Country: Japan. Propellants: Solid. Agency: Nissan.

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