This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Hyperion

Hyperion Interplanet
Hyperion Interplanet
Hyperion Interplanetary Spacecraft

Credit: © Mark Wade. 2,530 bytes. 455 x 125 pixels.


Family: Nerva. Country: USA. Status: Study 1959.

Hyperion was considered in 1958 as a ca. 1970 Saturn follow-on. It used a small jettisonable chemical booster stage that contained chemical engines and the LOX oxidizer for the conventional engines. This booster stage surrounded the nuclear core vehicle with its large liquid hydrogen tank. The conventional stage would draw fuel from the main hydrogen tank until burnout. Hyperion would have doubled the translunar trajectory performance of the Saturn V and less than one third of the liftoff mass.


Specifications

LEO Payload: 145,000 kg. to: 485 km Orbit. at: 28.0 degrees. Payload: 82,000 kg. to a: parabolic escape trajectory. Liftoff Thrust: 1,090,000 kgf. Total Mass: 850,000 kg. Core Diameter: 8.5 m. Total Length: 85.4 m.


Hyperion Chronology


- 1958 -

Bibliography:



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .