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.

All labels observed (1)

Label Occurrences
Atlas V 421 canonical 3

How this entity was disambiguated

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 ⓘ
countryOfOrigin United States ⓘ
designPurpose medium-class payloads to GTO and LEO ⓘ
fairingCodeDigit 4 ⓘ
fairingDiameter 4 meters ⓘ
fairingType 4 m short payload fairing ⓘ
family Atlas V ⓘ
familyCode 421 ⓘ
familyGeneration Atlas V 400 series ⓘ
firstStageName Common Core Booster ⓘ
guidanceSystem inertial guidance with GPS augmentation ⓘ
launchServiceProvider United Launch Alliance ⓘ
launchSitesUsed Cape Canaveral Space Force Station SLC-41 ⓘ
Vandenberg Space Force Base SLC-3E ⓘ
launchVehicleFamily Atlas family of launch vehicles ⓘ
launchVehicleType medium-lift launch vehicle ⓘ
manufacturer United Launch Alliance ⓘ
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 ⓘ
linked to: AJ-60 series
stages 2 ⓘ
status operational ⓘ
upperStage single-engine Centaur ⓘ
upperStageEngineCount 1 ⓘ
upperStageEngineType RL10 ⓘ
upperStageName Centaur ⓘ
usage U.S. government payload launches ⓘ
commercial satellite launches ⓘ

How these facts were elicited

Referenced by (3)

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