RS-36 Sustainer

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RS-36 Sustainer

Part of RS-36

RS-36 Sustainer
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. HOE Homing Overlay Experiment Upper Stage Axial Propulsion System. Pressure-fed. Derivative of Lance propulsion system. First flight 1983.

AKA: RS-36. Date: 1979. Thrust: 9.21 kN (2,070 lbf). Specific impulse: 262 s.

Country: USA. Launch Vehicles: HOE. Propellants: Lox/Kerosene. Agency: Rocketdyne.

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