E-1
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Boeing / Rocketdyne
Rocketdyne LOx/Kerosene rocket engine. Study 1957. Developed by USAF in late 1950's. Cancelled and decision to go direct to 1,500,000 lbf F-1 as next step. Booster applications. Gas generator, pump-fed.
Thrust (sl): 1,689.600 kN (379,837 lbf). Thrust (sl): 172,300 kgf. Propellant Formulation: Lox/RP-1.
Related
- Country
- USA
- Launch Vehicles
- Super-Jupiter
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne
Photo Gallery
E-1 Engine
Credit: © Mark Wade
