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 S-IB-4
Part of S-I stage Family
LOx/Kerosene propellant rocket stage. .

Status: Study 1960. Thrust: 30,962.53 kN (6,960,653 lbf). Gross mass: 1,813,729 kg (3,998,587 lb). Unfuelled mass: 108,823 kg (239,913 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 155 s. Height: 28.96 m (95.01 ft). Diameter: 10.06 m (33.00 ft). Span: 11.28 m (37.00 ft).

No Engines: 4.



Country: USA. Engines: F-1. Launch Vehicles: Saturn C-4. Propellants: Lox/Kerosene.

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