J-2T-250K
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Advanced Engines planned for uprated Saturn and Nova boosters
Credit: © Mark Wade
Rocketdyne LOx/LH2 rocket engine. Study 1967. Proposed for later versions of Saturn V. Toroidal aerospike plug nozzle version of J-2.
Thrust (sl): 731.000 kN (164,335 lbf). Thrust (sl): 74,544 kgf.
Related
- Country
- USA
- Launch Vehicles
- Saturn MLV-V-1/J-2T/250K, Saturn MLV-V-4(S)-B
- Propellants
- Lox/LH2
- Stages
- Saturn MS-II-1-J-2T-250K
- Agency
- Rocketdyne