ATCRE
Engine · Germany
Original archive entry. The text, images and links below are kept as they were written.
Notional LOx/LH2 rocket engine. Study 1985. Used on Sanger II launch vehicle.
Thrust (sl): 1,068.400 kN (240,186 lbf). Thrust (sl): 108,948 kgf. Chamber Pressure: 282.00 bar.
Related
- Country
- Germany
- Launch Vehicles
- Saenger II
- Propellants
- Lox/LH2
- Stages
- Sanger II-2