Plug-Nozzle Rombus
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1964. Used on Rombus launch vehicle.
Thrust (sl): 79,768.100 kN (17,932,582 lbf). Thrust (sl): 8,134,205 kgf.
Related
- Country
- USA
- Launch Vehicles
- Rombus
- Propellants
- Lox/LH2
- Stages
- Rombus core