XR3B4


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XR3B4
XCOR Nitrous oxide/Alcohol rocket engine. First stages. Hardware. Regeneratively cooled engine using nitrous oxide and isopropyl alcohol as propellants.

Status: Hardware. Date: 2000-2004. Thrust: 220 N (40 lbf).

The XCOR XR3B4 regeneratively cooled engine was capable of 220 newtons thrust, using nitrous oxide and isopropyl alcohol as propellants. This engine had completed 216 runs with a cumulative burn time of more than 812 seconds. XCOR designed this engine for use as a maneuvering thruster on spacecraft.

Country: USA. Propellants: Nitrous oxide/Alcohol. Agency: XCOR.
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