Saturn PFL

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 PFL

Part of Saturn LRB stage series

N2O4/UDMH propellant rocket stage. NASA, Saturn Alternative Booster Studies, 1969 (trade study of 120, 156, 260 inch solid, and Storable liquid boosters for S-IVB. Reached opposite conclusion from Boeing study, that Pressure Fed Liquid Booster would be 6.5% more expensive than solid). Pre.

Status: Study 1969. Thrust: 28,553.00 kN (6,418,969 lbf). Gross mass: 2,057,400 kg (4,535,700 lb). Unfuelled mass: 205,400 kg (452,800 lb). Specific impulse: 267 s. Specific impulse sea level: 245 s. Burn time: 167 s. Height: 33.57 m (110.13 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

Country: USA. Engines: PF N204/UDMH-2912k. Propellants: N2O4/UDMH.

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