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Expendable LV's

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Angara
Ariane 4
Ariane 5
Athena
Atlas II
Atlas III
Atlas V
Avrora (Aurora)
Beal BA-2
Delta II
Delta III
Delta IV
Dnepr
Eurockot
GSLV
H-IIA
J-1
Kosmos 3M
Long March 3
Pegasus
Proton
Shtil
Soyuz
Start
Strela
Taurus
Titan II
Titan IV
Tsiklon
Zenit

   Tsiklon - Summary
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The Tsikon launch vehicle (also knows as Tsyklon and Cyclone) was first introduced in 1966. It was derived from the R-36 ICBM (NATO designation of SS-9, Scarp). The earliest version was known as the R-36O, an orbital variant of the R-36, known as FOBS (Fractional Orbital Bombardment System), called fractional because the payloads reached orbit, but were to reenter over their targets prior to completing a full orbit. The first flight of the Tsiklon 2 was October 27, 1967, launching from Baikonur. The first flight of the Tsiklon 3, a Tsiklon 2 with a restartable third stage, first flew on June 27, 1977 from Plesetsk. 

Prime Contractor: KB Yuzhnoye/PO Yuzhmash, Dnepropetrovsk, Ukraine
Point of Contact
Fiat Avio
270 Sylvan Avenue
Englewood Cliffs, NJ 07632 USA
Launch Site: Tsiklon 2: LC 90 Pad 20 Baikonur Cosmodrome, Kazahkstan (46.1°N, 63.0°E)
Tsiklon 3: LC 32 Plesetsk Cosmodrome, Russia (62.7°N, 40.3°E)
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