Atlas V N22
E526120
Atlas V N22 is a specific variant of the Atlas V launch vehicle optimized for crewed missions, notably used to launch Boeing’s CST-100 Starliner spacecraft to low Earth orbit.
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
Atlas V rocket configuration
ⓘ
expendable launch system ⓘ orbital launch vehicle ⓘ |
| configurationCode | N22 NERFINISHED ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| crewCapacitySupported | up to 7 astronauts via Starliner ⓘ |
| crewSafetyFeature |
redundant avionics for crewed flight
ⓘ
upgraded emergency detection system ⓘ |
| customer |
Boeing
NERFINISHED
ⓘ
NASA NERFINISHED ⓘ |
| designedForDestination | International Space Station NERFINISHED ⓘ |
| fairingType | launch vehicle adapter and aeroskirt for Starliner ⓘ |
| firstStage | Atlas V Common Core Booster NERFINISHED ⓘ |
| firstStageEngine | RD-180 NERFINISHED ⓘ |
| firstStageEngineManufacturer | NPO Energomash NERFINISHED ⓘ |
| firstStageEngineType | liquid-fueled rocket engine ⓘ |
| firstStageOxidizer | liquid oxygen ⓘ |
| firstStagePropellant | RP-1 kerosene ⓘ |
| guidanceSystem | inertial guidance with GPS augmentation ⓘ |
| launchAzimuthRange | inclinations suitable for ISS rendezvous ⓘ |
| launchProfile | ascent trajectory tailored for Starliner abort modes ⓘ |
| launchSite | Cape Canaveral Space Force Station Space Launch Complex 41 NERFINISHED ⓘ |
| launchVehicleFamily | Atlas V NERFINISHED ⓘ |
| manufacturer | United Launch Alliance NERFINISHED ⓘ |
| missionRole | Commercial Crew Program launcher ⓘ |
| notableFeature |
first Atlas V variant certified for NASA crewed missions
ⓘ
only Atlas V configuration with dual-engine Centaur for crewed flights ⓘ |
| operator | United Launch Alliance NERFINISHED ⓘ |
| optimizedFor | crewed missions ⓘ |
| partOf | Atlas V family NERFINISHED ⓘ |
| primaryPayload | Boeing CST-100 Starliner NERFINISHED ⓘ |
| program | Atlas V program NERFINISHED ⓘ |
| propulsionType | liquid and solid propulsion combination ⓘ |
| reusability | non-reusable launch vehicle ⓘ |
| solidRocketBoosterManufacturer | Northrop Grumman NERFINISHED ⓘ |
| solidRocketBoosters | 2 ⓘ |
| solidRocketBoosterType | GEM-63 NERFINISHED ⓘ |
| stageCount | 2 ⓘ |
| status | operational during 2020s ⓘ |
| targetOrbit | low Earth orbit ⓘ |
| upperStage | Dual Engine Centaur NERFINISHED ⓘ |
| upperStageEngine | RL10A-4-2 NERFINISHED ⓘ |
| upperStageEngineManufacturer | Aerojet Rocketdyne NERFINISHED ⓘ |
| upperStageOxidizer | liquid oxygen ⓘ |
| upperStagePropellant | liquid hydrogen ⓘ |
| usedForMission |
Boe-OFT (Boeing Orbital Flight Test)
NERFINISHED
ⓘ
Boe-OFT-2 (Boeing Orbital Flight Test 2) NERFINISHED ⓘ Crew Flight Test (CFT) NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.