I2-BM

Overview

Destination: Low Earth Orbit
Mission: Government/Top Secret

Low Earth Orbit 90/19 Baikonur Cosmodrome, Republic of Kazakhstan

I2-BM was a mission to test the propulsion of the I2P coorbital ASAT satellite. It did not conduct any interception maneuveres.

Tsiklon-2A

Family:
Configuration: 2A

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 T
  • Thrust
    2366 kN
Family
  • Name
    Tsiklon-2A
  • Family
  • Variant
    2A
  • Alias
  • Full Name
    Tsiklon-2A
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    3000 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Yuzhnoye Design Bureau

Yuzhnoye Design Bureau

(OKB-586)

Director: Alexander Degtyarev Founded: 1951 Successes: 0 Failures: 0 Pending: 0

Agency Type:

Yuzhnoye 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.

INFO WIKI

Baikonur Cosmodrome, Republic of Kazakhstan

90/19


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