Ariane 2

Ariane 2
FunctionMedium launch vehicle
ManufacturerAérospatiale for
ESA and Arianespace
Size
Height49.13 m (161.2 ft)
Diameter3.8 m (12 ft)
Mass215,000 kg (474,000 lb)[1]
Stages3
Capacity
Payload to GTO
Mass2,175 kg (4,795 lb)[2]
Associated rockets
FamilyAriane
Launch history
StatusRetired
Launch sitesGuiana Space Centre ELA-1
Total launches6[2]
Success(es)5
Failure(s)1
First flight31 May 1986
Last flight2 April 1989
Type of passengers/cargoTele-X TV-SAT 1
First stage – L-140[3]
Height19.09 m (62.6 ft)
Diameter3.80 m (12.5 ft)
Gross mass165.89 tonnes (182.86 tons)
Powered byViking 5B
Maximum thrust2,580 kN (580,000 lbf)
Specific impulse2,376 N‑s/kg (242.3 s)
Burn time138 s
PropellantUH 25 / N2O4
Second stage – L-33[3]
Height11.47 m (37.6 ft)
Diameter2.60 m (8 ft 6 in)
Gross mass39.41 tonnes (43.44 tons)
Powered byViking 4B
Maximum thrust784.8 kN (176,400 lbf) (vacuum)
Specific impulse2,851 N‑s/kg (290.7 s)
Burn time128.9 s
PropellantUH 25 / N2O4
Third stage – H-10[3]
Height9.89 m (32.4 ft)
Diameter2.60 m (8 ft 6 in)
Gross mass12.74 tonnes (14.04 tons)
Powered byHM7B
Maximum thrust64.2 kN (14,400 lbf)
Specific impulse4,336 N‑s/kg (442.1 s)
Burn time729 s
PropellantLH2 / LOX

Ariane 2 was a European expendable space launch vehicle, operated by the European Space Agency (ESA) between 1986 and 1989 as part of Ariane family of rockets. The principal manufacturer for the Ariane 2 was Aérospatiale, while the lead agency for its development was the Centre National d'Etudes Spatiales (CNES), the French government's space agency.[4]

Development of the Ariane 2 was authorised in July 1979, months prior to the Ariane 1's first flight. Drawing heavily upon both the design and infrastructure of the Ariane 1, the new launcher was concurrently developed alongside the Ariane 3, with which it shared much of its design. It represented an advancement of the Ariane 1 rather than a replacement, but was capable of lifting even heavier payloads into Geostationary transfer orbit (GTO). Developed largely within a two-year window, the Ariane 2 performed its maiden flight on 31 May 1986, actually flying after its Ariane 3 sibling. During its brief service life, the final launch of the Ariane 2 having been conducted on 2 April 1989, the Ariane family had become increasingly commercially competitive, becoming the market leading heavy launch vehicle in the world by the late 1980s.

  1. ^ Harvey 2003, p. 518.
  2. ^ a b Krebs, Gunter. "Ariane-2". Gunter's Space Page. Retrieved 14 June 2015.
  3. ^ a b c "Ariane, Design(1)". b14643.de. Retrieved 13 June 2015.
  4. ^ Harvey 2003, p. 515.

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