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Engine Model: RJ47. Designer: Wright. Propellants: Air/Kerosene. Thrust(vac): 44.600 kN (10,026 lbf). Isp: 1,200 sec. Burn time: 10,300 sec. Chambers: 1. Country: USA. Status: Development ended 1958.

Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point.

Engine Model: XRJ47-W-5. Designer: Wright. Propellants: Air/Kerosene. Thrust(vac): 33.400 kN (7,509 lbf). Isp: 1,200 sec. Burn time: 6,500 sec. Chambers: 1. Country: USA. Status: Out of production. First Flight: 1956. Last Flight: 1958. Flown: 22.

Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point.

RJ47 used on Rocket Stages
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