RS-28 (original) (raw)

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RS-28

RS-28
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Space Shuttle Orbiter Reaction Control. Pressure-fed.

Date: 1972. Thrust: 2.67 kN (600 lbf). Specific impulse: 220 s.

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

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