VKS-RTO+ZhRD
Launch vehicle · Russia
Original archive entry. The text, images and links below are kept as they were written.
VKS with mixed propulsion
Russian winged orbital launch vehicle. Horizontal takeoff, delta winged, single-stage-to-orbit, launch vehicle. Mixed rocket / ramjet propulsion.
LEO Payload: 2,000 kg (4,400 lb) to a 200 km orbit at 51.00 degrees.
Related
- Family
- orbital launch vehicle, Winged
- Country
- Russia
- Agency
- Molniya bureau