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 MLV-V-1
Part of Saturn V
Saturn V-MLV-1
Saturn V-MLV-1
Credit: © Mark Wade
American orbital launch vehicle. MSFC study, 1965. Improved Saturn V configuration studied under contract NAS8-11359. Saturn IC stretched 240 inches with 5.6 million pounds propellant and 5 F-1A engines; S-II stretched 41 inches with 1.0 million pounds propellant and 5 J-2 engines; S-IVB strengthened but with standard 230,000 lbs propellant, 1 J-2 engine.

Status: Study 1965. Payload: 137,250 kg (302,580 lb). Thrust: 40,019.90 kN (8,996,831 lbf). Gross mass: 3,501,350 kg (7,719,150 lb). Height: 111.00 m (364.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 137,250 kg (302,580 lb) to a 185 km orbit at 28.00 degrees. Payload: 49,600 kg (109,300 lb) to a translunar trajectory.

Stage Data - Saturn MLV-V-1



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1A. Stages: Saturn MS-II-1, Saturn MS-IVB-1, Saturn MS-IC-1.
Photo Gallery

Saturn MLV 1.37Saturn MLV 1.37
Credit: © Mark Wade



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