Tsiklon-2A
In-activeYuzhnoye Design Bureau (OKB-586)
Oct. 27, 1967
Description
The Tsyklon was a Soviet-designed expendable launch system, primarily used to put Cosmos satellites into low Earth orbit. It is based on the R-36 intercontinental ballistic missile designed by Mikhail Yangel and made eight launches, with seven successes and one failure. All of its launches were conducted from LC-90 at the Baikonur Cosmodrome. It is sometimes designated Tsyklon-2A, not to be confused with the later Tsyklon-2 rocket. It was introduced in 1967 and was derived from the R-36 ICBM (NATO designation SS-9 Scarp). It was retired in 1969.
Specifications
-
Stages
2 -
Length
39.7 m -
Diameter
3.0 m -
Fairing Diameter
3.0 m -
Launch Mass
182.0 T -
Thrust
2366.0 kN
Family
-
Name
Tsiklon-2A -
Family
― -
Variant
2A -
Alias
― -
Full Name
Tsiklon-2A
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
3000.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
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.
Tsiklon-2A | US-AO 5
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Jan. 25, 1969, 11:14 a.m.
Status: Launch Failure
Mission:
US-A (Upravlenniye Sputnik Aktivny) were active radar satellites for ocean surveillance. The high power consumtion of the active radar required a nuclear reactor as power source. The satellites were known as RORSAT in the west. The US-AO series consisted of satellites, which tested all the system components but the nuclear reactor. They were battery powered.
Low Earth OrbitTsiklon-2A | I2P 2
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Nov. 1, 1968, 12:27 a.m.
Tsiklon-2A | I2P 1
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Oct. 20, 1968, 4:02 a.m.
Tsiklon-2A | I2M 2
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Oct. 19, 1968, 4:20 a.m.
Tsiklon-2A | I2M 1
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
April 24, 1968, 4 p.m.
Tsiklon-2A | US-AO 4
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
March 22, 1968, 9:30 a.m.
Status: Launch Successful
Mission:
US-A (Upravlenniye Sputnik Aktivny) were active radar satellites for ocean surveillance. The high power consumtion of the active radar required a nuclear reactor as power source. The satellites were known as RORSAT in the west. The US-AO series consisted of satellites, which tested all the system components but the nuclear reactor. They were battery powered.
Low Earth OrbitTsiklon-2A | US-AO 3
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Dec. 27, 1967, 11:28 a.m.
Status: Launch Successful
Mission:
US-A (Upravlenniye Sputnik Aktivny) were active radar satellites for ocean surveillance. The high power consumtion of the active radar required a nuclear reactor as power source. The satellites were known as RORSAT in the west. The US-AO series consisted of satellites, which tested all the system components but the nuclear reactor. They were battery powered.
Low Earth OrbitTsiklon-2A | I2-BM (Kosmos-185)
Yuzhnoye Design Bureau | UkraineBaikonur Cosmodrome, Republic of Kazakhstan
Oct. 27, 1967, 2:21 a.m.
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