Zenit-2
In-activeYuzhnoye Design Bureau (OKB-586)
April 13, 1985
Description
Zenit is a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union.
Specifications
-
Stages
2 -
Length
57.0 m -
Diameter
3.9 m -
Fairing Diameter
3.9 m -
Launch Mass
459.0 T -
Thrust
7300.0 kN
Family
-
Name
Zenit-2 -
Family
― -
Variant
2 -
Alias
― -
Full Name
Zenit-2
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
13740.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
5000.0 kg
Yuzhnoye Design Bureau
Commercial
Director: Alexander Degtyarev
OKB-586 1951Yuzhnoye Design Office, located in Dnipro, Ukraine, is a designer of satellites and rockets, and formerly of Soviet intercontinental ballistic missiles (ICBMs) established by Mikhail Yangel in 1951. The Zenit launch vehicle currently launches from Baikonur Cosmodrome but also used to launch from an ocean platform, Odyssey.
Flight Record
No spaceflights found for .
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