VKS-ZhRD+GPVRD (original) (raw)

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VKS-ZhRD+GPVRD

Part of VKS series

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.

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