Long March 2E

E729133

Long March 2E is a Chinese expendable orbital launch vehicle developed by the China Academy of Launch Vehicle Technology and used primarily in the 1990s to place communications satellites into geostationary transfer orbit.

All labels observed (1)

Label Occurrences
Long March 2E canonical 2

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf expendable orbital launch vehicle ⓘ
launch vehicle ⓘ
configuration two core stages plus four strap-on boosters and an upper stage ⓘ
countryOfOrigin China ⓘ
developer China Academy of Launch Vehicle Technology ⓘ
diameter 3.35 m (core stage) ⓘ
failedLaunches 2 ⓘ
failureCause fairing structural failure on some missions ⓘ
familyVariantOf Long March 2C ⓘ
firstFlightDate 1990-07-16 ⓘ
firstFlightPayload AsiaSat 1 ⓘ
firstStageOxidizer dinitrogen tetroxide ⓘ
firstStagePropellant unsymmetrical dimethylhydrazine ⓘ
hasBooster strap-on liquid rocket boosters ⓘ
height ~49.7 m ⓘ
introduced early 1990s ⓘ
lastFlightDate 1995-12-28 ⓘ
launchAzimuth optimized for GTO missions from Xichang ⓘ
launchEnvironment commercial satellite launch market ⓘ
launchMass ~460,000 kg ⓘ
launchPeriod 1990s ⓘ
launchSite Launch Area 2, Xichang Satellite Launch Center ⓘ
Launch Complex 2, Xichang Satellite Launch Center ⓘ
Xichang Satellite Launch Center ⓘ
manufacturer China Academy of Launch Vehicle Technology ⓘ
marketRole Chinese heavy-lift GTO launcher of the early 1990s ⓘ
notableFailure Apstar 2 launch failure ⓘ
Optus B2 launch failure ⓘ
numberOfStages 3 ⓘ
operator China Great Wall Industry Corporation ⓘ
China National Space Administration ⓘ
partOfFamily Long March 2 ⓘ
Long March rocket family ⓘ
payloadToGTO approximately 3,500 kg ⓘ
primaryOrbit geostationary transfer orbit ⓘ
primaryUse launching communications satellites ⓘ
propellantType hypergolic propellants ⓘ
retiredFromService mid-1990s ⓘ
secondStageOxidizer dinitrogen tetroxide ⓘ
secondStagePropellant unsymmetrical dimethylhydrazine ⓘ
status retired ⓘ
successfulLaunches 5 ⓘ
successor Long March 3B ⓘ
totalLaunches 7 ⓘ
upperStageType solid-propellant upper stage ⓘ
usedFor international commercial satellite launches ⓘ
launching foreign-built communications satellites ⓘ

How these facts were elicited

Referenced by (2)

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