Saturn IVB (S-V)

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 IVB (S-V)

Part of Saturn IV

LOx/LH2 propellant rocket stage. Saturn V version of S-IVB stage for use with upper stage.

Status: Study 1968. Thrust: 1,031.60 kN (231,913 lbf). Gross mass: 119,900 kg (264,300 lb). Unfuelled mass: 13,300 kg (29,300 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 475 s. Height: 17.80 m (58.30 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Country: USA. Engines: J-2. Launch Vehicles: Saturn V 2, Saturn INT-20, Saturn V-A, Saturn V-C, Saturn V-D, Saturn V-Centaur. 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