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VKS-RTO+ZhRD
Part of VKS series
VKS - Mixed
VKS - Mixed
VKS with mixed propulsion
Russian winged orbital launch vehicle. Horizontal takeoff, delta winged, single-stage-to-orbit, launch vehicle. Mixed rocket / ramjet propulsion.

Status: Study 1988. Payload: 2,000 kg (4,400 lb). Gross mass: 770,000 kg (1,690,000 lb). Apogee: 200 km (120 mi).

LEO Payload: 2,000 kg (4,400 lb) to a 200 km orbit at 51.00 degrees.

Family: orbital launch vehicle, Winged. Country: Russia. Agency: Molniya bureau.
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