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-II-C3
Part of Saturn II Family
LOx/LH2 propellant rocket stage. Version for Saturn C-3.

Status: Study 1960. Thrust: 3,557.31 kN (799,716 lbf). Gross mass: 204,044 kg (449,840 lb). Unfuelled mass: 24,938 kg (54,978 lb). Specific impulse: 420 s. Specific impulse sea level: 300 s. Burn time: 200 s. Height: 21.30 m (69.80 ft). Diameter: 8.25 m (27.06 ft). Span: 8.25 m (27.06 ft).

No Engines: 4.



Country: USA. Engines: J-2. Launch Vehicles: Saturn C-3. 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use