J-2T-200K
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 1965. Proposed for later versions of Saturn V. Toroidal aerospike plug nozzle version of J-2.
Thrust (sl): 613.300 kN (137,875 lbf). Thrust (sl): 62,542 kgf.
Related
- Country
- USA
- Launch Vehicles
- Saturn MLV-V-1/J-2T/200K
- Propellants
- Lox/LH2
- Stages
- Saturn MS-II-1-J-2T-200K
- Agency
- Rocketdyne