RS-36

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RS-36

RS-36 Sustainer
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. HOE Homing Overlay Experiment Upper Stage Axial Propulsion System. Pressure-fed. Derivative of Lance propulsion system. First flight 1983.

Date: 1979. Thrust: 55.60 kN (12,499 lbf). Specific impulse: 281 s.

Subtopics

RS-36 Sustainer Rocketdyne LOx/Kerosene rocket engine. HOE Homing Overlay Experiment Upper Stage Axial Propulsion System. Pressure-fed. Derivative of Lance propulsion system. First flight 1983.

Family: Storable liquid. Country: USA. Launch Vehicles: HOE. Propellants: N2O4/MMH. Agency: Rocketdyne.

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