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
Saturn MS-II-1-J-2T-250K
Part of Saturn II
LOx/LH2 propellant rocket stage. Basic Saturn II with 41 inch stretch of hydrogen tank, uprated J-2T 250k engines with 25% improvement in thrust and 16 second increase in specific impulse.
Status: Study 1967. Thrust: 5,558.31 kN (1,249,558 lbf). Gross mass: 521,447 kg (1,149,593 lb). Unfuelled mass: 49,877 kg (109,959 lb). Specific impulse: 441 s. Specific impulse sea level: 290 s. Burn time: 348 s. Height: 25.88 m (84.90 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).
No Engines: 5.
Country:
USA.
Engines:
J-2T-250K.
Launch Vehicles:
Saturn MLV-V-1/J-2T/250K,
Saturn MLV-V-4(S)-B.
Propellants:
Lox/LH2.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use