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Soyuz 11A510
Part of R-7
Russian orbital launch vehicle. Version of R-7 launch vehicle with Vostok second stage and unknown third stage used only twice to launch prototype RORSATs. These satellites were originally to have been launched on the cancelled UR-200 launcher, and operational satellites used Tsyklon-2 launchers.

AKA: 11A510;A;SL-5;Vostok 11A510. Status: Retired 1966. First Launch: 1965-12-27. Last Launch: 1966-07-20. Number: 2 . Payload: 4,500 kg (9,900 lb). Thrust: 4,037.70 kN (907,711 lbf). Gross mass: 275,000 kg (606,000 lb). Height: 31.00 m (101.00 ft). Diameter: 10.30 m (33.70 ft). Apogee: 200 km (120 mi).

LEO Payload: 4,500 kg (9,900 lb) to a 200 km orbit at 65.00 degrees.

Stage Data - Vostok 11A510



Family: orbital launch vehicle. Country: Russia. Spacecraft: US-A. Projects: RORSAT. Launch Sites: Baikonur, Baikonur LC31. Stages: Vostok 8A92-2, Soyuz 11A511-0, Soyuz 11A511-1, Tsyklon 2-3. Agency: Korolev bureau.

1965 December 27 - . 22:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A510.
1966 July 20 - . 09:07 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A510.

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