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XR5M12
XCOR LOx/CH4 rocket engine. First stages. Conceptual LOx/methane rocket engine developed for a DARPA program through layout design phase, but never built.

Status: Hardware. Date: 2004-2006. Thrust: 22.30 kN (5,013 lbf).

The DARPA contract enabled XCOR to develop the methane cooling analysis tools used in later engine designs.

Country: USA. Propellants: Lox/LCH4. Agency: XCOR.
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