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-IVB-1A
Part of Saturn IV
LOx/LH2 propellant rocket stage. S-IVB with 16.5 foot stretch, 350,000 pounds propellant, standard J-2 engine.

Status: Study 1967. Thrust: 1,031.60 kN (231,913 lbf). Gross mass: 179,200 kg (395,000 lb). Unfuelled mass: 20,400 kg (44,900 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 625 s. Height: 22.82 m (74.86 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).



Family: Space Tugs. Country: USA. Engines: J-2. Launch Vehicles: Saturn MLV-V-1A, Saturn V-ELV, Saturn V-23(L), Saturn V-24(L), Saturn V-25(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