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
Jupiter (stage)
LOx/Kerosene propellant rocket stage. .

AKA: Jupiter. Status: Retired 1963. Thrust: 758.71 kN (170,565 lbf). Gross mass: 54,431 kg (119,999 lb). Unfuelled mass: 5,443 kg (11,999 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 182 s. Height: 18.28 m (59.97 ft). Diameter: 2.67 m (8.75 ft). Span: 2.67 m (8.75 ft).

Cost $ : 7.830 million.



Country: USA. Engines: S-3. Launch Vehicles: Jupiter IRBM, Juno II, Juno II (3). 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