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Truax LH2
Aerojet LOx/LH2 rocket engine. Test 1962. Used in Sea Horse-2.

Status: Test 1962. Thrust: 147.10 kN (33,069 lbf). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 363 s. Diameter: 3.00 m (9.80 ft).

Thrust (sl): 105.900 kN (23,807 lbf). Thrust (sl): 10,800 kgf.

Country: USA. Launch Vehicles: Sea Horse. Propellants: Lox/LH2. Stages: Sea Horse-2. Agency: Aerojet.



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