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RS-14
RS-14
RS-14
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/MMH rocket engine. Minuteman Postboost Velocity Control. Pressure-fed. First flight 1970.

Date: 1966. Thrust: 1.39 kN (313 lbf). Specific impulse: 315 s.



Subtopics

RS-1402 Rocketdyne N2O4/MMH rocket engine. Minuteman Pitch, Yaw & Roll Control. Pressure-fed. Technology engine, developed, but not produced. Led to RS-14 production engines.

RS-1403 Rocketdyne N2O4/MMH rocket engine. Minuteman Pitch, Yaw & Roll Control. Pressure-fed. Technology engine, developed, but not produced. Led to RS-14 production engines.

RS-2101A Rocketdyne N2O4/MMH rocket engine. Mars Mariner. Pressure-fed. Derivative of RS-14 Minuteman engine. First flight 1971.

RS-2101C Rocketdyne N2O4/MMH rocket engine. Viking. Pressure-fed. Derivative of RS-14 Minuteman engine. First flight 1975.

RS-32 Rocketdyne N2O4/MMH rocket engine. Upper Stage Target Engine Systems. Pressure-fed. Derived from Minuteman RS-14.

RS-2101 Rocketdyne N2O4/MMH rocket engine. Derivative of RS-14 Minuteman engine.

Family: Storable liquid. Country: USA. Launch Vehicles: Minuteman 3. Propellants: N2O4/MMH. Stages: PBS. Agency: Rocketdyne.

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