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VKS-ZhRD+GPVRD
Part of VKS series
VKS - Rocket
VKS - Rocket
VKS pure rocket propulsion version.
Russian winged orbital launch vehicle. Horizontal takeoff, delta winged, single-stage-to-orbit, launch vehicle. Mixed rocket / scramjet propulsion.

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

to: 200 km orbit at 51.00 degrees.

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