Atlas V 421

E525240

Atlas V 421 is a specific medium-lift configuration of the Atlas V launch vehicle, featuring a 4-meter payload fairing, two 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
boosterCodeDigit 2
centaurEngineCodeDigit 1
configurationFeatures 4-meter payload fairing
single-engine Centaur upper stage
two strap-on solid rocket boosters
coreStageEngineType RD-180 NERFINISHED
countryOfOrigin United States of America
surface form: United States
designPurpose medium-class payloads to GTO and LEO
fairingCodeDigit 4
fairingDiameter 4 meters
fairingType 4 m short payload fairing
family Atlas V NERFINISHED
familyCode 421
familyGeneration Atlas V 400 series NERFINISHED
firstStageName Common Core Booster NERFINISHED
guidanceSystem inertial guidance with GPS augmentation
launchServiceProvider United Launch Alliance NERFINISHED
launchSitesUsed Cape Canaveral Space Force Station SLC-41 NERFINISHED
Vandenberg Space Force Base SLC-3E NERFINISHED
launchVehicleFamily Atlas family of launch vehicles
launchVehicleType medium-lift launch vehicle
manufacturer United Launch Alliance NERFINISHED
missionTypes Earth-orbit missions
communications satellite launches
military payload launches
numberOfSolidRocketBoosters 2
payloadFairingDiameter 4-meter payload fairing
propellantTypeFirstStage RP-1/LOX
propellantTypeUpperStage LH2/LOX
solidRocketBoosterType AJ-60A NERFINISHED
stages 2
status operational
upperStage single-engine Centaur
upperStageEngineCount 1
upperStageEngineType RL10 NERFINISHED
upperStageName Centaur NERFINISHED
usage U.S. government payload launches
commercial satellite launches

Referenced by (1)

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Atlas V configurationOptions Atlas V 421