A-10 engine
Engine · Germany
Original archive entry. The text, images and links below are kept as they were written.
Thiel LOx/Alcohol rocket engine. Study 1942. Planned for use in A-10. Unique dual-thrust chamber / single nozzle design, which was later shown to be not feasible technically.
Thrust (sl): 1,961.300 kN (200,000 kgf / 440,918 lbf).
Related
- Country
- Germany
- Launch Vehicles
- A9/A10, A9/A10/A11
- Propellants
- Lox/Alcohol
- Agency
- Thiel