Atlas V 511

E525651

Atlas V 511 is a specific medium-lift configuration of the Atlas V expendable launch vehicle, distinguished by its single solid rocket booster and five-meter payload fairing.

All labels observed (1)

Label Occurrences
Atlas V 511 canonical 3

How this entity was disambiguated

Statements (32)

Predicate Object
instanceOf Atlas V rocket configuration
expendable launch vehicle configuration
configurationCodeMeaning first digit indicates payload fairing diameter in meters
second digit indicates number of solid rocket boosters
third digit indicates number of Centaur engines
coreEngine RD-180
coreEngineType liquid-fueled rocket engine
corePropellants RP-1 and liquid oxygen
coreStage Common Core Booster
countryOfOrigin United States
designFeature dual-engine Centaur option not used
five-meter payload fairing
single solid rocket booster
fairingManufacturer RUAG Space
launchProvider United Launch Alliance
launchSites Cape Canaveral Space Force Station
Vandenberg Space Force Base
launchVehicleFamily Atlas V
liftClass medium-lift launch vehicle
manufacturer United Launch Alliance
missionProfile orbital launch missions
namingScheme Atlas V three-digit configuration code
partOf Atlas V family
linked to: Atlas V
payloadFairingDiameter 5 meters
payloadFairingType 5-meter payload fairing
solidRocketBoosters 1
staging two-stage with optional solid booster
status operational
upperStage Centaur
upperStageEngines 1
upperStageEngineType RL10
upperStagePropellants liquid hydrogen and liquid oxygen

How these facts were elicited

Referenced by (3)

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

Atlas V configurationOptions Atlas V 511
Atlas V 500 series familyIncludes Atlas V 511