Atlas V 411
E525198
Atlas V 411 is a specific variant of the Atlas V expendable launch vehicle characterized by a single solid rocket booster and a four-meter payload fairing, used to place satellites and spacecraft into orbit.
Statements (47)
| Predicate | Object |
|---|---|
| instanceOf |
Atlas V launch vehicle variant
ⓘ
expendable launch vehicle ⓘ |
| boosterCountClass | single-booster configuration ⓘ |
| capability |
placing satellites into orbit
ⓘ
placing spacecraft into orbit ⓘ |
| configurationCode | 411 ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| designFeature |
4-meter payload fairing
ⓘ
single solid rocket booster ⓘ |
| designPurpose | medium-lift missions ⓘ |
| fairingDiameterClass | medium ⓘ |
| familyDeveloper | Lockheed Martin NERFINISHED ⓘ |
| familyIntroductionYear | 2002 ⓘ |
| firstStageEngine | RD-180 NERFINISHED ⓘ |
| firstStageEngineType | liquid-fueled rocket engine ⓘ |
| firstStageOxidizer | liquid oxygen ⓘ |
| firstStagePropellant | RP-1 ⓘ |
| firstStageType | Common Core Booster NERFINISHED ⓘ |
| launchesPayloadsFor |
NASA
NERFINISHED
ⓘ
U.S. Department of Defense NERFINISHED ⓘ commercial customers ⓘ |
| launchPad | Space Launch Complex 41 NERFINISHED ⓘ |
| launchSitesUsed |
Cape Canaveral Space Force Station
NERFINISHED
ⓘ
Vandenberg Space Force Base NERFINISHED ⓘ |
| launchVehicleFamily | Atlas V NERFINISHED ⓘ |
| launchVehicleSeries | Evolved Expendable Launch Vehicle program NERFINISHED ⓘ |
| manufacturer | United Launch Alliance NERFINISHED ⓘ |
| numberOfSolidRocketBoosters | 1 ⓘ |
| operator | United Launch Alliance NERFINISHED ⓘ |
| orbitTypes |
geostationary transfer orbit
ⓘ
highly elliptical orbit ⓘ low Earth orbit ⓘ |
| partOf | Atlas V family NERFINISHED ⓘ |
| payloadFairingDiameter | 4 meters ⓘ |
| payloadFairingType | 4-meter payload fairing ⓘ |
| propellantCombination |
LH2/LOX upper stage
ⓘ
RP-1/LOX first stage ⓘ |
| propulsionType | liquid and solid propulsion ⓘ |
| solidRocketBoosterType | GEM-63 NERFINISHED ⓘ |
| stages | 2 ⓘ |
| status | operational ⓘ |
| upperStageEngine | RL10 NERFINISHED ⓘ |
| upperStageEngineType | cryogenic rocket engine ⓘ |
| upperStageOxidizer | liquid oxygen ⓘ |
| upperStagePropellant | liquid hydrogen ⓘ |
| upperStageType | Centaur NERFINISHED ⓘ |
| usage | orbital launch vehicle ⓘ |
Referenced by (3)
Full triples — surface form annotated when it differs from this entity's canonical label.
subject surface form:
OSIRIS-REx