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
Super-Jupiter-2
LOx/Kerosene propellant rocket stage. .

AKA: Saturn E-1. Status: Development 1958. Thrust: 1,884.59 kN (423,673 lbf). Gross mass: 96,700 kg (213,100 lb). Unfuelled mass: 7,200 kg (15,800 lb). Specific impulse: 290 s. Specific impulse sea level: 260 s. Burn time: 133 s. Height: 18.00 m (59.00 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).



Country: USA. Engines: E-1. 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