Wright ramjet engine. 44.6 kN. Development ended 1958. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Isp=1200s. Used on Navaho G-38 launch vehicle.
Status: Development ended 1958.
More... - Chronology...
Thrust: 44.60 kN (10,026 lbf).
Specific impulse: 1,200 s.
Burn time: 10,300 s.
Associated Launch Vehicles
Navaho G-38 American intercontinental cruise missile. The intercontinental-range Navaho G-38 was the ultimate development of the German A-9/A-10 concept. At the time the Navaho program was cancelled on 13 July 1957 missiles were in fabrication with first flight test planned by the end of 1958. More...
Associated Manufacturers and Agencies
Wright American manufacturer of rocket engines. Wright, USA. More...
Air/Kerosene Ambient air (78 % nitrogen, 21% oxygen, etc.) is scooped up by air intakes and used in turbojet, turbofan, ramjet, scramjet, or other airbreathing engines. It is used to burn aviation-grade kerosene, commercial grade JP-4 or JP-5, their military equivalents, or special high-temperature blends such as those used in the SR-71. More...
Navaho G-38 Ramjet-powered missile stage. Loaded/empty mass 54,648/14,512 kg. Thrust 89.26 kN. Specific impulse 1200 seconds. Separates from booster at 21,600 m, Mach 3. Mach 3.25 cruise, 10,200 km range, payload 4545 kg in 3.76 m x 1.78 m weapons bay. Empty mass estimated. More...
Home - Browse - Contact
© / Conditions for Use