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 5-23L-0
Part of Saturn LRB stage series
LOx/Kerosene propellant rocket stage. Liquid strap-on booster studied for improved Saturn V.

Status: Study 1966. Thrust: 15,484.00 kN (3,480,941 lbf). Gross mass: 1,180,000 kg (2,600,000 lb). Unfuelled mass: 80,000 kg (176,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 200 s. Height: 51.00 m (167.00 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

No Engines: 2.



Country: USA. Engines: F-1. Propellants: Lox/Kerosene.

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