Atlas V 400 series

E1010995

The Atlas V 400 series is a configuration of the Atlas V expendable launch vehicle family that uses a four-meter payload fairing and optional solid rocket boosters to deliver a wide range of payloads to orbit.

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Statements (42)

Predicate Object
instanceOf Atlas V configuration
launch vehicle configuration
canUseUpToNumberOfSRBs 3
configurationCodePattern 4xx
countryOfOrigin United States of America
surface form: United States
designFeature 4-meter class payload fairing for smaller payloads
exampleConfiguration Atlas V 401 NERFINISHED
Atlas V 411 NERFINISHED
Atlas V 421 NERFINISHED
Atlas V 431 NERFINISHED
fairingDiameter 4.2 meters
fairingType extended 4-m fairing
short 4-m fairing
familyRole medium-lift launch vehicle configuration
firstStageEngine RD-180 NERFINISHED
firstStagePropellant RP-1/LOX
hasOptionalComponent solid rocket booster
launchCapability geostationary transfer orbit
highly elliptical orbit
interplanetary trajectory
low Earth orbit
launchProvider United Launch Alliance NERFINISHED
launchSite Cape Canaveral Space Force Station NERFINISHED
Vandenberg Space Force Base NERFINISHED
manufacturer United Launch Alliance NERFINISHED
operator United Launch Alliance NERFINISHED
partOf Atlas V family NERFINISHED
propulsionType liquid-fueled core with optional solid boosters
rocketFamily Atlas V NERFINISHED
secondStageEngine RL10 NERFINISHED
secondStagePropellant LH2/LOX
staging two-stage
status operational
usedFor U.S. government payloads
commercial satellite launches
interplanetary missions
military payloads
scientific missions
usesFirstStage Common Core Booster NERFINISHED
usesPayloadFairingDiameter 4 meters
usesPayloadFairingType 4-meter payload fairing
usesSecondStage Centaur NERFINISHED

Referenced by (2)

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

AJ-60A solid rocket booster usedOnVariant Atlas V 400 series