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H1500
Notional LOx/Solid hybrid rocket engine. Design 1988. Used on Industrial Launch Vehicle launch vehicle.

Status: Design 1988. Thrust: 931.30 kN (209,365 lbf). Specific impulse: 284 s. Specific impulse sea level: 283 s. Burn time: 75 s. Diameter: 1.83 m (6.00 ft).

Thrust (sl): 928.000 kN (208,622 lbf). Thrust (sl): 94,636 kgf.

Family: Hybrid. Country: USA. Engines: H1500. Launch Vehicles: Industrial Launch Vehicle, AMROC IRR. Propellants: Lox/Solid. Stages: AMROC Aquila.
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