Jump to content

Ariane 2

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Chobot (talk | contribs) at 00:24, 24 October 2009 (robot Adding: ro:Ariane 2). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Ariane 2
FunctionCarrier rocket
ManufacturerAérospatiale
Arianespace
Country of origin Europe
Size
Height49 metres (161 ft)
Diameter3.8 metres (12 ft)
Mass217,000 kilograms (478,000 lb)
StagesThree
Capacity
Payload to GTO
Mass2,175 kilograms (4,795 lb)
Associated rockets
FamilyAriane
Derivative workAriane 3
Launch history
StatusRetired
Total launches6
Success(es)5
Failure(s)1
First flight31 May 1986
Last flight2 April 1989

Ariane 2 was a European expendable carrier rocket, which was used for six launches between 1986 and 1989. It was a member of the Ariane family of rockets, and was produced by Aérospatiale in France.

The Ariane 2 was derived from the earlier Ariane 1, with stretched first and third stages. Its payload capacity was increased to 2,175 kilograms (4,795 lb) to a geosynchronous transfer orbit. It first flew on 31 May 1986 carrying the Intelsat-5A F-14 satellite. The third stage failed to ignite, and the rocket was destroyed by range safety. Following this, five more launches were conducted, all of which were successful. The last Ariane 2 launch occurred on 2 April 1989, successfully placing Tele-X into orbit.


References

  • "Ariane 1, 2, 3". Launchers. European Space Agency. Retrieved 2009-04-27.
  • "Ariane 1-3". Ariane Heritage. Arianespace. Retrieved 2009-04-27.
  • Krebs, Gunter. "Ariane-2". Gunter's Space Page. Retrieved 2009-04-27.
  • Wade, Mark. "Ariane". Encyclopedia Astronautica. Retrieved 2009-04-27.