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 SSTO stage
LOx/LH2 propellant rocket stage. All values estimated based on drawing, statement that 5 x mass of SASSTO, payload performance, and 300 m/s sled velocity augmentation.
AKA: Hyperion SSTO. Status: Study 1968. Thrust: 7,840.00 kN (1,762,500 lbf). Gross mass: 450,000 kg (990,000 lb). Unfuelled mass: 44,000 kg (97,000 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 300 s. Height: 18.00 m (59.00 ft). Diameter: 10.00 m (32.00 ft). Span: 16.00 m (52.00 ft).
Cost $ : 40.000 million. dV Equivalent: 500 m/s (1,640 ft/sec). Release conditions: 1,080 kph at sea level.
Country:
USA.
Launch Vehicles:
Hyperion SSTO.
Propellants:
Lox/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