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.

All labels observed (1)

Label Occurrences
Atlas V 400 series canonical 5

How this entity was disambiguated

Statements (42)

Predicate Object
instanceOf Atlas V configuration
launch vehicle configuration
canUseUpToNumberOfSRBs 3
configurationCodePattern 4xx
countryOfOrigin United States
designFeature 4-meter class payload fairing for smaller payloads
exampleConfiguration Atlas V 401
Atlas V 411
Atlas V 421
Atlas V 431
fairingDiameter 4.2 meters
fairingType extended 4-m fairing
short 4-m fairing
familyRole medium-lift launch vehicle configuration
firstStageEngine RD-180
firstStagePropellant RP-1/LOX
hasOptionalComponent solid rocket booster
launchCapability geostationary transfer orbit
highly elliptical orbit
interplanetary trajectory
low Earth orbit
launchProvider United Launch Alliance
launchSite Cape Canaveral Space Force Station
Vandenberg Space Force Base
manufacturer United Launch Alliance
operator United Launch Alliance
partOf Atlas V family
linked to: Atlas V
propulsionType liquid-fueled core with optional solid boosters
rocketFamily Atlas V
secondStageEngine RL10
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
usesPayloadFairingDiameter 4 meters
usesPayloadFairingType 4-meter payload fairing
usesSecondStage Centaur

How these facts were elicited

Referenced by (5)

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

AJ-60A solid rocket booster usedOnVariant Atlas V 400 series
RD-180 poweredVehicleFamily Atlas V 400 series
Atlas V 421 familyGeneration Atlas V 400 series