Encyclopedia Astronautica
Soyuz 11A514



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Soyuz LV
Credit: © Mark Wade
Russian orbital launch vehicle. Version of Soyuz launcher with increased payload, designed to launch Soyuz R military reconnaisance satellite. Cancelled along with the Soyuz R project in 1966. Unknown differences to standard Soyuz to reach payload requirement of circa 6700 kg to 65 degree orbit.

LEO Payload: 6,700 kg (14,700 lb) to a 200 km orbit at 65.00 degrees.

AKA: Vostok; SL-4; 11A514; Sapwood; A-2.
Status: Development ended 1966.
Payload: 6,700 kg (14,700 lb).
Apogee: 200 km (120 mi).

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Associated Countries
Associated Spacecraft
  • Soyuz VI Russian manned combat spacecraft. Cancelled 1965. To determine the usefulness of manned military space flight, two projects were pursued in the second half of the 1960's. More...

See also
  • R-7 The world's first ICBM became the most often used and most reliable launch vehicle in history. The original core+four strap-on booster missile had a small third stage added to produce the Vostok launch vehicle, with a payload of 5 metric tons. Addition of a larger third stage produced the Voskhod/Soyuz vehicle, with a payload over 6 metric tons. Using this with a fourth stage, the resulting Molniya booster placed communications satellites and early lunar and planetary probes in higher energy trajectories. By the year 2000 over 1,628 had been launched with an unmatched success rate of 97.5% for production models. Improved models providing commercial launch services for international customers entered service in the new millenium, and a new launch pad at Kourou was to be inaugurated in 2011. It appeared that the R-7 could easily still be in service 70 years after its first launch. More...

Associated Manufacturers and Agencies
  • Korolev Russian manufacturer of rockets, spacecraft, and rocket engines. Korolev Design Bureau, Kaliningrad, Russia. More...

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