RS-71

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RS-71

RS-71
Credit: Boeing / Rocketdyne

Rocketdyne LOx/LH2 rocket engine. Development ended 1999. Linear Aerospike SR-71 Experiment. Pressure-fed.

Status: Development ended 1999. Date: 1998. Thrust: 31.13 kN (6,997 lbf). Specific impulse: 430 s.

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

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