Delta III

E722100

Delta III was an American expendable launch vehicle developed in the late 1990s as an upgraded, higher-capacity member of the Delta rocket family, intended primarily for launching communications satellites to geostationary orbit.

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Statements (45)

Predicate Object
instanceOf expendable launch vehicle
orbital launch vehicle
alsoKnownAs Delta 8930 configuration
configuration two-stage rocket with optional third stage
coreStageEngine RS-27A NERFINISHED
countryOfOrigin United States of America
surface form: United States
designFeature more powerful solid rocket boosters
new cryogenic upper stage
stretched first stage
designGoal higher capacity than Delta II
developedInPeriod late 1990s
diameter 4 meters
era post–Cold War space launchers
failedLaunches 2
fairingDiameter 4 meters
firstFlightDate 1998-08-26
firstLaunchOutcome failure
firstLaunchPayload Galaxy 10 NERFINISHED
gtoPayloadCapacity approximately 3,800 kilograms
height about 38.7 meters
intendedOrbit geostationary transfer orbit
intendedUse launching communications satellites
lastFlightDate 2000-08-23
launchFamilyPredecessor Delta II NERFINISHED
launchSite Cape Canaveral Air Station Space Launch Complex 17B NERFINISHED
launchVehicleFamily Delta NERFINISHED
manufacturer Boeing
McDonnell Douglas NERFINISHED
numberOfSolidBoosters 9
operator Boeing NERFINISHED
partOf Delta rocket family NERFINISHED
propellantTypeFirstStage RP-1/LOX
propellantTypeUpperStage liquid hydrogen/liquid oxygen
retirementReason poor reliability record
secondLaunchOutcome failure
secondLaunchPayload Orion 3 NERFINISHED
solidBoostersType GEM-46 NERFINISHED
status retired
successfulLaunches 1
successor Delta IV NERFINISHED
thirdLaunchOutcome partial failure
thirdLaunchPayload BSAT-2b NERFINISHED
totalLaunches 3
upperStageEngine RL10B-2 NERFINISHED
usedBy commercial satellite operators

Referenced by (2)

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

Delta rocket hasVariant Delta III
Delta IV predecessor Delta III