This page no longer updated from 31 October 2001. Latest version can be found at Nova MM S10R-2

Nova Model S10R-2
Nova Model S10R-2 - Nova Martin Marietta Model S10R-2

Credit: © Mark Wade. 2,720 bytes. 156 x 391 pixels.

Family: Nova. Country: USA. Status: Study 1963.

Reusable single stage to orbit Nova using conical shape, 30 CD module engines in zero-length plug nozzle. Operational date would have been July 1978.


LEO Payload: 381,000 kg. to: 185 km Orbit. at: 0.0 degrees. Liftoff Thrust: 13,605,220 kgf. Total Mass: 10,959,200 kg. Core Diameter: 21.3 m. Total Length: 68.0 m.


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Last update 12 March 2001.
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© Mark Wade, 2001 .