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.
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 NERFINISHED ⓘ |
| coreEngineType | liquid-fueled rocket engine ⓘ |
| corePropellants | RP-1 and liquid oxygen ⓘ |
| coreStage | Common Core Booster NERFINISHED ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| designFeature |
dual-engine Centaur option not used
ⓘ
five-meter payload fairing ⓘ single solid rocket booster ⓘ |
| fairingManufacturer | RUAG Space NERFINISHED ⓘ |
| launchProvider | United Launch Alliance NERFINISHED ⓘ |
| launchSites |
Cape Canaveral Space Force Station
NERFINISHED
ⓘ
Vandenberg Space Force Base NERFINISHED ⓘ |
| launchVehicleFamily | Atlas V NERFINISHED ⓘ |
| liftClass | medium-lift launch vehicle ⓘ |
| manufacturer | United Launch Alliance NERFINISHED ⓘ |
| missionProfile | orbital launch missions ⓘ |
| namingScheme | Atlas V three-digit configuration code ⓘ |
| partOf | Atlas V family NERFINISHED ⓘ |
| payloadFairingDiameter | 5 meters ⓘ |
| payloadFairingType | 5-meter payload fairing ⓘ |
| solidRocketBoosters | 1 ⓘ |
| staging | two-stage with optional solid booster ⓘ |
| status | operational ⓘ |
| upperStage | Centaur NERFINISHED ⓘ |
| upperStageEngines | 1 ⓘ |
| upperStageEngineType | RL10 NERFINISHED ⓘ |
| upperStagePropellants | liquid hydrogen and liquid oxygen ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.