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Пуск РН «Протон-М» с КА Eutelsat 5 West B и Mission Extension Vehicle-1

9 октября 2019 года в 13:17:56 на космодроме Байконур состоялся пуск ракеты космического назначения "Протон-М" с телекоммуникационным спутником Eutelsat 5 We...

ILS - E5WB MEV-1

Launch was scheduled 06:17 EDT on October 9th; 10:17 GMT on October 9th. Broadcast began at 06:00 EDT on October 9th; 10:00 GMT on October 9th.

Eutelsat 5 West B & MEV-1

Overview

Destination: Geostationary Transfer Orbit
Mission: Communications

Geostationary Transfer Orbit 200/39 (200L) Baikonur Cosmodrome, Republic of Kazakhstan

Eutelsat 5 West B will replace the Ku-band capacity of Eutelsat 5 West A (formerly Stellat 5) satellite, a key digital infrastructure addressing predominantly French, Italian and Algerian broadcast markets. Eutelsat 5 West B will provide business continuity and improved quality for these services via a Ku-band payload. The satellite is built on Orbital ATKs GEOStar-2e bus and carries 35 equivalent 36 MHz Ku-band transponders connected to three service areas. Switchable transponders will also increase commercial flexibility. Co-passenger on this flight will be provided Northrop Grumman Innovation Systems. MEV-1 (Mission Extension Vehicle-1) incorporates flight-proven technologies the company has used in its commercial satellite and space logistics businesses. After successfully completing a series of in-orbit tests, the MEV-1 will begin its mission extension service for Intelsat-901 satellite in the graveyard orbit. MEV-1 will relocate the satellite scheduled for the mission extension service, which is planned for a five-year period, after which Intelsat 901 will be place back into graveyard orbit. Intelsat will also have the option to service multiple satellites using the same MEV. MEV-1 is based on the company’s GEOStar-3 spacecraft bus platform. Controlled by the company’s satellite operations team, the MEV-1 uses a reliable, low-risk docking system that attaches to existing features on a customer’s satellite. The MEV-1 provides life-extending services by taking over the propulsion and attitude control functions. The vehicle has a 15-year design life with the ability to perform numerous dockings and undockings during its life span.

Proton-M Briz-M

Family: Proton
Configuration: Briz-M

Specifications
  • Minimum Stage
    1
  • Max Stage
    4
  • Length
    53.0 m
  • Diameter
    7.4 m
  • Fairing Diameter
  • Launch Mass
    712 T
  • Thrust
    10000 kN
Family
  • Name
    Proton-M Briz-M
  • Family
    Proton
  • Variant
    Briz-M
  • Alias
  • Full Name
    Proton-M Briz-M
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    21000 kg
  • Geostationary Transfer Orbit
    4500 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity

Khrunichev State Research and Production Space Center

Circle Image
Director: Andrey Vladimirovich Kalinovskiy Founded: 1916 Successes: 86 Failures: 9 Pending: 11

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

Baikonur Cosmodrome, Republic of Kazakhstan

Pad: 200/39 (200L)


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