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Reaction Motors XLR11

Rocket engine
The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed and built by Reaction Motors Inc., and used ethyl alcohol and liquid oxygen as propellants... Wikipedia
Dry weight: 210 lb (95 kg)
Propellant: LOX / Ethyl alcohol
Thrust: 6,000 lbf (27 kN)