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-LRB-23(L)
Part of Saturn LRB stage series Family
LOx/Kerosene propellant rocket stage. Liquid rocket booster strap-ons using 2 F-1's.

Status: Study 1967. Thrust: 15,486.60 kN (3,481,526 lbf). Gross mass: 874,100 kg (1,927,000 lb). Unfuelled mass: 18,100 kg (39,900 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 162 s. Height: 47.85 m (156.98 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

No Engines: 2.



Country: USA. Engines: F-1. Launch Vehicles: Saturn V-23(L), Saturn V-24(L). Propellants: Lox/Kerosene.

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