Arianespace Ariane 1 1979 - Hero viewArianespace Ariane 1 1979 - Top View viewArianespace Ariane 1 1979 - Profile viewArianespace Ariane 1 1979 - Bottom View viewArianespace Ariane 1 1979 - Avionics Bay viewArianespace Ariane 1 1979 - Fairing viewArianespace Ariane 1 1979 - H8 viewArianespace Ariane 1 1979 - L140 viewArianespace Ariane 1 1979 - Fairing viewArianespace Ariane 1 1979 - Hm7 viewArianespace Ariane 1 1979 - Interstage viewArianespace Ariane 1 1979 - Viking view
Hero
First of its kind

The first European orbital launch vehicle, giving Europe independent access to space. Ariane 1 launched from Kourou, French Guiana, establishing the equatorial launch site that remains Europe''s spaceport today.

History

Ariane 1 was born from European determination to achieve independent access to space without relying on American or Soviet rockets. Development began in the early 1970s under French leadership, with contributions from ten European nations.

The three-stage rocket used Viking engines burning UDMH and nitrogen tetroxide on its first and second stages, and a cryogenic HM7 engine burning liquid hydrogen and liquid oxygen on its third stage. The choice of the Guiana Space Centre in Kourou, French Guiana, as the launch site provided the advantage of being near the equator, giving rockets a significant boost from Earth''s rotation.

Ariane 1''s first flight on December 24, 1979, was successful, placing a test satellite in orbit. It went on to fly 11 missions between 1979 and 1986, with 9 successes. While its payload capacity was modest compared to American and Soviet rockets, Ariane 1 established Europe as an independent spacefaring entity and laid the foundation for the commercially dominant Ariane 4 and Ariane 5 that followed.

Timeline

1979First flight
1986It went on to fly 11 missions between 1979 and 1986, with 9 successes

Launch Heritage

Operational StatusRetired
Total Launches9/11 (82%)
Service Period1979-1986
DesignerCNES / Airbus
Mission TypeSatellite delivery
ReusabilityExpendable
Orbit TypeLEO
Target BodyEarth
Production Total11
Notable Missions
  • CAT-1 L01
  • Giotto
  • SPOT 1

Technical Specifications

PropulsionLiquid (UDMH + LH2)
Height155.5 ft
Length155.5 ft
Diameter/Wingspan12.5 ft
Gross Mass462,970 lbs

Propulsion

Engine ModelViking 5 (first/second stage) + HM7 (third stage)
Engine Count5
Engine ManufacturerSEP / Snecma
Thrust2771 kN
Specific Impulse281 s
PropellantN2O4/UDMH (stages 1-2) + LH2/LOX (stage 3)
Stages3

Performance

Payload to LEO1,830 kg
Payload to GTO1,010 kg

Dimensions

Height (m)47.4 m
Diameter (m)3.8 m
Length (m)47.4 m

Mass

Empty Mass (kg)13,500 kg
Gross Mass (kg)210,000 kg

Mission

Mission Duration11 launches (1979-1986), 9 successes
Missions Flown11
Success Rate9/11
ReusableNo

Power & Systems

AvionicsInertial guidance platform, onboard computer for staging
Communication BandS-band telemetry, C-band tracking

Tags

Designed by CNES / Airbus

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