Ariane 2

E412129

Ariane 2 was a European expendable launch vehicle developed by the European Space Agency as part of the Ariane family, used in the 1980s primarily to place satellites into geostationary transfer orbit.

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All labels observed (1)

Label Occurrences
Ariane 2 canonical 6

Statements (49)

Predicate Object
instanceOf Ariane rocket
expendable launch vehicle
orbital launch vehicle
commercialOperator Arianespace
configuration three-stage launch vehicle
countryOfOrigin Europe
France
developer CNES
surface form: Centre National d'Études Spatiales

European Space Agency
diameter about 3.8 m
era 1980s
failedLaunches 1
familyVariantOf Ariane 1
firstFlightDate 1986-05-31
firstFlightLocation Kourou
surface form: Kourou, French Guiana
firstStageEngineType Viking engine
firstStagePropellants N2O4
UDMH
height about 49 m
lastFlightDate 1989-04-02
lastFlightLocation Kourou
surface form: Kourou, French Guiana
launchAgency European Space Agency
launchFailureCount 1
launchLocation Kourou
surface form: Kourou, French Guiana
launchMass approximately 210000 kg
launchPad ELA-1
launchSite Guiana Space Centre
manufacturer Aérospatiale
notableFailure first launch failure on 1986-05-31
operator Arianespace
partOf Ariane family
payloadToGTO about 2175 kg
payloadToLEO about 4700 kg
primaryMissionType communications satellite launch
propellantTypeFirstStage hypergolic
propellantTypeSecondStage hypergolic
propellantTypeThirdStage cryogenic
secondStagePropellants N2O4
UDMH
stageCount 3
status retired
successfulLaunches 5
successor Ariane 4
thirdStageEngineType HM7 engine
surface form: HM7B engine
thirdStagePropellants liquid hydrogen
liquid oxygen
totalLaunches 6
usedForOrbitType geostationary transfer orbit
low Earth orbit

Referenced by (6)

Full triples — surface form annotated when it differs from this entity's canonical label.