Status: Development ended 1958. Thrust: 44.60 kN (10,026 lbf). Specific impulse: 1,200 s. Burn time: 10,300 s.
XRJ47-W-5 Wright ramjet engine. Out of production. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Used on Navaho G-26 launch vehicle. First flight 1956. |