Skip to content
EntityQ18375· pop 30· linked from 579 articles

rocket of the Ariane family

Key facts

Function
Medium lift launch vehicle
Manufacturer
Aérospatiale
Country of origin
France
Height
50 m (160 ft)
Diameter
3.8 m (12 ft)
Mass
207,200 kg (456,800 lb)
Status
Retired
Launch sites
ELA-1 , Guiana Space Centre
First flight
24 December 1979
Last flight
22 February 1986
Carries passengers or cargo
Giotto
Powered by
4 Viking-5
Maximum thrust
2,771.940 kN (623,157 lbf)
Specific impulse
281 s (2.76 km/s)
Burn time
145 seconds
Propellant
N 2 O 4 / UDMH

via Wikipedia infobox

Wikidata facts

Diameter
3.8
Mass
207200
Image
Ariane 1 Le Bourget FRA 001.jpg
Height
47.4
Show 4 more facts
Commons category
Ariane 1
start time
1979-12-24
end time
1986-02-22
payload mass
1830
Sources (4)

via Wikidata · CC0

~12 min read

Article

Ariane 1 ( French: [aʁjan œ̃]) was the first rocket in the Ariane family of expendable launch systems. It was developed for and operated by the European Space Agency (ESA), which had been formed in 1973, the same year that development of the launcher had commenced. Aérospatiale was designated to lead the programme. 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. 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.

Connections

Categories