Atlas V 431

E525429

Atlas V 431 is a specific medium-lift configuration of the Atlas V launch vehicle, featuring a 4-meter payload fairing, three solid rocket boosters, and a single-engine Centaur upper stage.

All labels observed (1)

Label Occurrences
Atlas V 431 canonical 2

How this entity was disambiguated

Statements (40)

Predicate Object
instanceOf Atlas V launch vehicle configuration ⓘ
expendable launch system ⓘ
codeFirstDigitMeaning 4-meter payload fairing ⓘ
codeSecondDigitMeaning 3 solid rocket boosters ⓘ
codeThirdDigitMeaning 1 Centaur engine ⓘ
coreStageEngineCount 1 ⓘ
coreStageEngineType RD-180 ⓘ
coreStageOrigin Atlas III heritage ⓘ
linked to: Atlas III
countryOfOrigin United States ⓘ
designFeature 4-meter class payload fairing ⓘ
single-engine Centaur upper stage ⓘ
strap-on solid rocket boosters ⓘ
familyDesignationCode 431 ⓘ
familyDeveloper Lockheed Martin ⓘ
familyFirstFlight Atlas V first flew in 2002 ⓘ
guidanceSystem inertial guidance ⓘ
launchAzimuthFlexibility supports multiple inclinations ⓘ
launchSitesUsed Cape Canaveral Space Force Station SLC-41 ⓘ
Vandenberg Space Force Base SLC-3E ⓘ
launchVehicleFamily Atlas V ⓘ
launchVehicleRole orbital launch vehicle ⓘ
liftCapabilityClass medium-lift ⓘ
manufacturer United Launch Alliance ⓘ
numberOfSolidRocketBoosters 3 ⓘ
operator United Launch Alliance ⓘ
payloadFairingDiameter 4-meter ⓘ
payloadFairingType 4-meter payload fairing ⓘ
propellantCoreStage RP-1/LOX ⓘ
propellantUpperStage LH2/LOX ⓘ
solidRocketBoosterType AJ-60A ⓘ
linked to: AJ-60 series
stages 2 ⓘ
status operational ⓘ
typicalMissions communications satellite launches ⓘ
typicalOrbitTypes GTO ⓘ
LEO ⓘ
upperStage Centaur ⓘ
upperStageEngineCount 1 ⓘ
upperStageEngineModel RL10A-4-2 ⓘ
linked to: RL10
upperStageEngineType RL10 ⓘ
upperStageHeritage Centaur upper stage family ⓘ
linked to: Centaur upper stage

How these facts were elicited

Referenced by (2)

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