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
Helios C-2
Part of Helios A-2 Family
Nuclear/LH2 propellant rocket stage. Nuclear second stage.

Status: Study 1960. Thrust: 5,780.00 kN (1,299,390 lbf). Gross mass: 309,000 kg (681,000 lb). Unfuelled mass: 54,000 kg (119,000 lb). Specific impulse: 830 s. Burn time: 355 s. Height: 85.40 m (280.10 ft). Diameter: 8.50 m (27.80 ft). Span: 12.20 m (40.00 ft).

No Engines: 2.



Country: USA. Engines: Nuclear 12 Gw. Launch Vehicles: Helios C. Propellants: Nuclear/LH2.

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