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XR3A2
XCOR LOx/Alcohol rocket engine. First stages. Hardware. The XR3A2 700-newton engine was the first XCOR LOX/alcohol engine, accumulating 61 brief runs in the course of injector concept development, which led to later engines.

Status: Hardware. Date: 2000-2004. Thrust: 700 N (150 lbf).



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

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