This page no longer updated from 31 October 2001.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

astronautix.com Nova 5S

Nova NASA 5 Solids
Nova NASA 5 Solids - Nova NASA 5 Solid Motors

Credit: © Mark Wade. 1,689 bytes. 50 x 442 pixels.



Family: Nova. Country: USA. Status: Study, NASA, 1960.

Nova design using segmented solid motors in first and second stages. Five six segment motors in first stage; four four segment motors in second stage, equivalent to 9 x F-1 first stage and 4 x F-1 second stage.


Specifications

LEO Payload: 176,000 kg. to: 160 km Orbit. at: 0.0 degrees. Payload: 59,000 kg. to a: translunar trajectory. Liftoff Thrust: 12,927,100 kgf. Total Mass: 10,076,200 kg. Core Diameter: 10.1 m. Total Length: 147.0 m.


Nova 5S Chronology


1961 Jun 23 -

Bibliography:



Nova Concepts - NASANova Concepts - NASA

Credit: © Mark Wade. 13,422 bytes. 640 x 349 pixels.



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 .