Watch the Launch

ExoMars Trace Gas Orbiter & EDM Schiaparelli lander

Overview

Destination: Heliocentric N/A
Mission: Planetary Science

Heliocentric N/A 200/39 (200L) Baikonur Cosmodrome, Republic of Kazakhstan

This is the first part of ESA’s and Roscosmos’s Mars exploration programme (ExoMars). The launch in the 2016 Mars window will consist of an orbiter and lander and will take 7 months to travel to Mars. The Trace Gas Orbiter will search for trace gases in the atmosphere such as methane and hydrogen. The Schiaparelli lander will travel with the orbiter until each reaches Mars, where it will attempt to descend through the atmosphere and land on the surface. The lander only contains a small array of scientific instruments, to conduct experiments over 4 Martian days.

Proton-M Briz-M

Family: Proton / UR-500
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 / UR-500
  • 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: 178 Failures: 15 Pending: 4

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

200/39 (200L)


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