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Engine Model: Truax LH2. Propellants: Lox/LH2. Thrust(vac): 147.100 kN (33,069 lbf). Thrust(sl): 105.900 kN (23,807 lbf). Isp: 425 sec. Isp (sea level): 306 sec. Burn time: 363 sec. Diameter: 3.00 m (9.80 ft). Chambers: 1. Country: USA. Status: Test 1962. Used in Sea Horse-2.
Truax LH2 used on Rocket Stages
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