Glonass-M (Kosmos 2500)

Overview

Destination: Medium Earth Orbit
Mission: Navigation

Medium Earth Orbit 43/4 (43R) Plesetsk Cosmodrome, Russian Federation

Glonass-M, also known as Uragan-M, are the second generation of Uragan satellite design used for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system comparable to the similar GPS and Galileo systems. This generation improves on accuracy, power consumption and design life. Each satellite weighs 1415 kg, is equipped with 12 L-band antennas, and has an operational lifetime of 7 years.

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Soyuz 2.1B

Family: Soyuz
Configuration: Fregat

Soyuz-2, GRAU index 14A14, is the collective designation for the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The first-stage boosters and two core stages feature uprated engines with improved injection systems, compared to the previous versions of the Soyuz. Digital flight control and telemetry systems allow the rocket to be launched from a fixed launch platform, whereas the launch platforms for earlier Soyuz rockets had to be rotated as the rocket could not perform a roll to change its heading in flight. The Soyuz 2.1b represents the latest development stage of the proven rocket. It uses the new RD-0124 engines in the first three stages, coupled with an improved injection system that significantly boosts the performance of the Soyuz. Furthermore, she wears a new, digital startup control system. This will allow the Soyuz 2.1b to carry around 1.2 tonnes more payload into low earth orbit compared to its predecessor.

Specifications
  • Minimum Stage
    3
  • Max Stage
    4
  • Length
    46.3 m
  • Diameter
    2.95 m
  • Fairing Diameter
    4.11 m
  • Launch Mass
    312 T
  • Thrust
    4150 kN
Family
  • Name
    Soyuz 2.1B
  • Family
    Soyuz
  • Variant
    Fregat
  • Alias
  • Full Name
    Soyuz 2.1B Fregat
Payload Capacity
  • Launch Cost
    $80M
  • Low Earth Orbit
    8200 kg
  • Geostationary Transfer Orbit
    3250 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity
    4900 kg

Khrunichev State Research and Production Space Center

Circle Image
Director: Andrey Vladimirovich Kalinovskiy Founded: 1916 Successes: 85 Failures: 9 Pending: 12

Agency Type: Government

Khrunichev State Research and Production Space Center is a Moscow-based producer of spacecraft and space-launch systems, including the Proton and Rokot rockets and is currently developing the Angara rocket family. The Proton launch vehicle launches from Baikonur and Rokot launches from Baikonur and Plesetsk. Angara will launch from Plesetsk and Vostochny.

INFO WIKI

Plesetsk Cosmodrome, Russian Federation

Pad: 43/4 (43R)


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