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.

All labels observed (1)

Label Occurrences
Atlas V N22 canonical 3

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf Atlas V rocket configuration ⓘ
expendable launch system ⓘ
orbital launch vehicle ⓘ
configurationCode N22 ⓘ
countryOfOrigin United States ⓘ
crewCapacitySupported up to 7 astronauts via Starliner ⓘ
crewSafetyFeature redundant avionics for crewed flight ⓘ
upgraded emergency detection system ⓘ
customer Boeing ⓘ
NASA ⓘ
designedForDestination International Space Station ⓘ
fairingType launch vehicle adapter and aeroskirt for Starliner ⓘ
firstStage Atlas V Common Core Booster ⓘ
linked to: Common Core Booster
firstStageEngine RD-180 ⓘ
firstStageEngineManufacturer NPO Energomash ⓘ
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 ⓘ
launchVehicleFamily Atlas V ⓘ
manufacturer United Launch Alliance ⓘ
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 ⓘ
optimizedFor crewed missions ⓘ
partOf Atlas V family ⓘ
linked to: Atlas V
primaryPayload Boeing CST-100 Starliner ⓘ
program Atlas V program ⓘ
linked to: Atlas V
propulsionType liquid and solid propulsion combination ⓘ
reusability non-reusable launch vehicle ⓘ
solidRocketBoosterManufacturer Northrop Grumman ⓘ
solidRocketBoosters 2 ⓘ
solidRocketBoosterType GEM-63 ⓘ
linked to: GEM 63XL
stageCount 2 ⓘ
status operational during 2020s ⓘ
targetOrbit low Earth orbit ⓘ
upperStage Dual Engine Centaur ⓘ
linked to: Centaur upper stage
upperStageEngine RL10A-4-2 ⓘ
linked to: RL10
upperStageEngineManufacturer Aerojet Rocketdyne ⓘ
upperStageOxidizer liquid oxygen ⓘ
upperStagePropellant liquid hydrogen ⓘ
usedForMission Boe-OFT (Boeing Orbital Flight Test) ⓘ
Boe-OFT-2 (Boeing Orbital Flight Test 2) ⓘ
Crew Flight Test (CFT) ⓘ

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 N22 ⓘ
OFT → launchVehicle → Atlas V N22 ⓘ