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.

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

Referenced by (1)

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Atlas V configurationOptions Atlas V 431