| Voskhod (R-7 11A57) | |||||||||||||||||||
| Function: | Crew-rated LEO carrier rocket | ||||||||||||||||||
| Manufacturer: | OKB-1 | ||||||||||||||||||
| Country-Origin: | Soviet Union | ||||||||||||||||||
| Stages: | 2 | ||||||||||||||||||
| Capacities: | |||||||||||||||||||
| Family: | R-7 | ||||||||||||||||||
| Status: | Retired | ||||||||||||||||||
| Sites: | Baikonur Site 1 and Site 31 Plesetsk, Site 41 | ||||||||||||||||||
| First: | 16 November 1963 | ||||||||||||||||||
| Last: | 29 June 1976 | ||||||||||||||||||
| Launches: | 300 | ||||||||||||||||||
| Success: | 287 | ||||||||||||||||||
| Fail: | 13 | ||||||||||||||||||
| Payloads: | Voskhod spacecraft Zenit (satellite) | ||||||||||||||||||
| Stagedata: |
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The Voskhod rocket (Russian: Восход, "ascent", "dawn") was a derivative of the Soviet R-7 ICBM designed for the human spaceflight programme but later used for launching Zenit reconnaissance satellites.[1] [2] It consisted of the Molniya 8K78M third stage minus the Blok L.[3] In 1966, all R-7 variants were equipped with the uprated core stage and strap-ons of the Soyuz 11A511. The Blok I stage in the Voskhod booster used the RD-0107 engine rather than the crew-rated and more powerful RD-0110 used on the Soyuz. The sole exceptions to this were the two crewed Voskhod launches, which had RD-0108 engines, a crew-rated RD-0107 but with the same performance.
All 11A57s launched after 1965 were functionally 11A511s without the Soyuz's payload shroud and launch escape system (with the exception of the second-stage propulsion system as noted above). Around 300 were flown from Baikonur and Plesetsk through 1976 (various payloads, but Zenith IMINT satellites were the most common). The newer 11A511U core had been introduced in 1973, but the existing stock of 11A57s took another three years to use up.
The rocket had a streak of 86 consecutive successful launches between 11 September 1967 and 9 July 1970.