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LH2 2000/3000 lbf thrust
Aerojet LOx/LH2 rocket engine. Development begun July 1946. Engine R&D, hydrogen production

Date: July 1946. Thrust: 13.33 kN (2,997 lbf).

Thrust (sl): 13.330 kN (2,997 lbf). Thrust (sl): 1,360 kgf.



Country: USA. Propellants: Lox/LH2. Agency: Aerojet.

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