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RS-X

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RS-X
Rocketdyne LOx/Kerosene rocket engine. Design concept -1997. Employed existing Delta and Atlas MA and RS engine hardware with a new thrust chamber assembly to generate a thrust of 1890 kN for ELV applications.
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Status: Design concept -1997. Thrust: 1,890.00 kN (424,880 lbf).

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

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