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A-10 engine
Part of A-10 Family
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.

AKA: A-10. Status: Study 1942. Thrust: 2,306.80 kN (518,589 lbf). Specific impulse: 247 s. Specific impulse sea level: 210 s. Burn time: 55 s. Diameter: 4.12 m (13.51 ft).

Thrust (sl): 1,961.300 kN (200,000 kgf / 440,918 lbf).



Country: Germany. Launch Vehicles: A9/A10, A9/A10/A11. Propellants: Lox/Alcohol. Stages: A-10, A-11, A-12. Agency: Thiel.

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