Arabsat 4A

Overview

Destination: Geostationary Orbit
Mission: Communications

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

The Arabsat-4 spacecraft are based on the Eurostar-2000+ version of the Eurostar satellite family. Both satellites received the names Badr-1 and Badr-4 respectively in February 2006. Badr 1 did not reach its planned orbit, when the upper stage of the Proton-M Briz-M (Ph.3) launch vehicle failed. After evaluating a lunar fly-by maneuvre to rescue the satellite, Badr 1 was deorbited on 24.03.2006 over the pacific.

Proton-M Briz-M

Family:
Configuration: Briz-M

Specifications
  • Minimum Stage
    1
  • Max Stage
    4
  • Length
    53.0 m
  • Diameter
    7.4 m
  • Fairing Diameter
  • Launch Mass
    712.0 T
  • Thrust
    10000.0 kN
Family
  • Name
    Proton-M Briz-M
  • Family
  • Variant
    Briz-M
  • Alias
  • Full Name
    Proton-M Briz-M
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    21000.0 kg
  • Geostationary Transfer Orbit
    4500.0 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity

Khrunichev State Research and Production Space Center

Khrunichev State Research and Production Space Center

(KhSC)

Director: Andrey Vladimirovich Kalinovskiy Founded: 1916 Successes: 180 Failures: 15 Pending: 1

Agency Type:

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

200/39 (200L)


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