![]() Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z J-2T-200K ![]() Advanced Engines Advanced Engines planned for uprated Saturn and Nova boosters Credit: © Mark Wade Status: Study 1965. Thrust: 889.30 kN (199,923 lbf). Specific impulse: 435 s. Specific impulse sea level: 300 s. Burn time: 429 s. Height: 1.25 m (4.10 ft). Diameter: 2.49 m (8.16 ft). Thrust (sl): 613.300 kN (137,875 lbf). Thrust (sl): 62,542 kgf.
Country: USA. Launch Vehicles: Saturn MLV-V-1/J-2T/200K. Propellants: Lox/LH2. Stages: Saturn MS-II-1-J-2T-200K. Agency: Rocketdyne. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2017 Mark Wade - Contact © / Conditions for Use |
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