Q1526424: Difference between revisions
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Latest revision as of 13:17, 17 February 2025
The Voskhod rocket was Soviet medium-lift launch vehicle, a derivative of the R-7, an ICBM. The Voskhod rocket was designed for the human spaceflight programme but later used for launching Zenit reconnaissance satellites. It was essentially an 8K78/8K78M minus the Blok L stage and spec-wise was a halfway between the two boosters, with the former's older, lower-spec engines and the latter's improved Blok I design. Its first flight was on 16 November 1963 when it successfully launched a Zenit satellite from LC-1/5 at Baikonur. Boosters used in the Voskhod program had a man-rated version of the RD-0107 engine; this version was known as the RD-0108.
1963 — 1976
Wikimedia, Wikidata
Voskhod rocket
height 3084 centimetre, diameter 299 centimetre, payload mass 5900 kilogram, mass 298400 kilogram,
S.P. Korolev Rocket and Space Corporation Energia,
Dong Fang Hong 2, Ekran, expendable launch vehicle, R-7, 1963, [[Voskhod|]],
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Location: KML, Cluster Map, Maps,
Voshod-rocket| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Voshod-rocket | Commons | ||
