Saturn II-SL

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 II-SL

Part of Saturn II

LOx/LH2 propellant rocket stage. Saturn II modified with reduced expansion ratio J-2 engines for use a first stage (sea level launch). Requires solid rocket motor augmentation to get off the ground.

Status: Study 1966. Thrust: 5,500.77 kN (1,236,621 lbf). Gross mass: 490,952 kg (1,082,363 lb). Unfuelled mass: 44,240 kg (97,530 lb). Specific impulse: 390 s. Specific impulse sea level: 275 s. Burn time: 310 s. Height: 24.84 m (81.49 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.

Country: USA. Engines: J-2-SL. Launch Vehicles: Saturn INT-19. Propellants: Lox/LH2.

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