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
Hyperion Sustainer
Part of Hyperion
Nuclear/LH2 propellant rocket stage. .

Status: Study 1959. Thrust: 5,782.68 kN (1,299,998 lbf). Gross mass: 453,592 kg (999,999 lb). Unfuelled mass: 110,000 kg (240,000 lb). Specific impulse: 800 s. Burn time: 460 s. Height: 51.00 m (167.00 ft). Diameter: 8.54 m (28.01 ft). Span: 8.54 m (28.01 ft).

No Engines: 2.



Country: USA. Engines: Nerva 12 GW. Launch Vehicles: Hyperion 1958. Propellants: Nuclear/LH2.

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