VKS-G

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VKS-G

Part of VKS series

Russian winged orbital launch vehicle. Air launched from Kholod Mach 5 mother ship. This was a Mikoyan supersonic cargo aircraft, designed from Spiral 50-50 design. Combined-cycle turbo-ramjet engine. Release conditions: Piggy-back, 200,000 kg, Mach 5 at 25 to 30 km altitude. Effective velocity gain compared to vertical launch 1130 m/s. It was concluded that the extensive development would be required for the combination-cycle engines, resulting in an extended development schedule and high technical risk. The more conservative subsonic-launched MAKS was chosen instead.

Status: Study 1988. Payload: 21,000 kg (46,000 lb). Apogee: 200 km (120 mi).

LEO Payload: 21,000 kg (46,000 lb) to a 200 km orbit at 51.00 degrees.

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

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