Ariane 1

Ariane 1
Ariane 1 mock-up (Photo taken at Musée de l'Air et de l'Espace, Le Bourget, France)
FunctionMedium lift launch vehicle
ManufacturerAérospatiale
Country of originEuropean Space Agency
Size
Height50 m (160 ft)
Diameter3.8 m (12 ft)
Mass207,200 kg (456,800 lb)
Stages3
Capacity
Payload to LEO
Mass4,850 kilograms (10,690 lb)
Payload to GTO
Mass1,850 kilograms (4,080 lb)
Launch history
StatusRetired
Launch sitesELA-1, Guiana Space Centre
Total launches11
Success(es)9
Failure(s)2
First flight24 December 1979
Last flight22 February 1986
Type of passengers/cargoGiotto
First stage
Powered by4 Viking-5
Maximum thrust2,771.940 kN (623,157 lbf)
Specific impulse281 s (2.76 km/s)
Burn time145 seconds
PropellantN2O4 / UDMH
Second stage
Powered by1 Viking-4
Maximum thrust720.965 kN (162,079 lbf)
Specific impulse296 s (2.90 km/s)
Burn time132 seconds
PropellantN2O4 / UDMH
Third stage
Powered by1 HM7-A
Maximum thrust61.674 kN (13,865 lbf)
Specific impulse443 s (4.34 km/s)
Burn time563 seconds
PropellantLH2 / LOX

Ariane 1 was the first rocket in the Ariane family of expendable launch systems. It was developed and operated by the European Space Agency (ESA), which had been formed in 1973, the same year that development of the launcher had commenced.

Ariane 1 was the first launcher to be developed with the primary purpose of sending commercial satellites into geosynchronous orbit. Crucially, it was designed with the ability of sending a pair of satellites into orbit on a single launcher, thus reducing costs. As the size of satellites grew, Ariane 1 quickly gave way to the more powerful Ariane 2 and Ariane 3 launchers, which were heavily based upon the original rocket.[1] The Ariane 4 was the last rocket to heavily draw upon the Ariane 1, as the successor rocket Ariane 5 uses a far greater proportion of all-new elements.

  1. ^ "Ariane 1,2,3". Ariane 1. ESA. 2004-05-04. Archived from the original on 2012-09-06. Retrieved 2009-09-28.

© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search