MB-3-J
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: © Mark Wade
Rocketdyne LOx/Kerosene rocket engine. N Booster . Gas generator, pump-fed. Joint MHI (Japan) / Rocketdyne project, evolved from MB-3. Thrust and specific impulse values are at sea level. First flight 1975.
Thrust (sl): 755.890 kN (169,931 lbf). Thrust (sl): 77,080 kgf. Propellant Formulation: Lox/RP-1.
Related
- Country
- USA
- Propellants
- Lox/Kerosene
- Agency
- Rocketdyne