H1500
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/Solid hybrid rocket engine. Design 1988. Used on Industrial Launch Vehicle launch vehicle.
Thrust (sl): 928.000 kN (208,622 lbf). Thrust (sl): 94,636 kgf.
Related
- Family
- Hybrid
- Country
- USA
- Engines
- H1500
- Launch Vehicles
- Industrial Launch Vehicle, AMROC IRR
- Propellants
- Lox/Solid
- Stages
- AMROC Aquila