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astronautix.com VKS-RTO+ZhRD

VKS - Mixed
VKS - Mixed
VKS with mixed propulsion

7,175 bytes. 468 x 138 pixels.


Family: Winged. Country: USSR. Status: Study 1988.

Horizontal takeoff, delta winged, single-stage-to-orbit, launch vehicle. Mixed rocket / ramjet propulsion.


Specifications

LEO Payload: 2,000 kg. to: 200 km Orbit. at: 51.0 degrees. Total Mass: 770,000 kg.



Bibliography:



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Last update 12 March 2001.
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