Pegasus XL

E239143

Pegasus XL is an air-launched, three-stage solid-fuel orbital rocket developed by Orbital Sciences Corporation for placing small satellites into low Earth orbit.

All labels observed (3)

Label Occurrences
Pegasus XL canonical 14
Pegasus H 1
Pegasus air-launched rocket 1

How this entity was disambiguated

Statements (50)

Predicate Object
instanceOf air-launched rocket ⓘ
expendable launch vehicle ⓘ
orbital launch vehicle ⓘ
carrierAircraftName Stargazer ⓘ
carrierAircraftType Lockheed L-1011 TriStar ⓘ
countryOfOrigin United States ⓘ
developer Orbital Sciences Corporation ⓘ
diameter approximately 1.27 m ⓘ
fairingType payload fairing ⓘ
family Pegasus rocket family ⓘ
firstFlightDate 1994-06-27 ⓘ
firstStageName Orion 50SXL ⓘ
guidanceSystem inertial guidance ⓘ
improvementOver original Pegasus design ⓘ
intendedOrbit low Earth orbit ⓘ
launchAzimuthFlexibility high ⓘ
launchEnvironmentAdvantage ability to avoid bad weather at ground sites ⓘ
reduced atmospheric drag at ignition ⓘ
launchMass approximately 23,000 kg ⓘ
launchMethod air launch ⓘ
launchPlatform Stargazer L-1011 ⓘ
launchServiceProvider Northrop Grumman ⓘ
Orbital ATK ⓘ
Orbital Sciences Corporation ⓘ
launchSites air-launched near Cape Canaveral ⓘ
air-launched near Vandenberg Air Force Base ⓘ
air-launched over Atlantic Ocean ⓘ
air-launched over Pacific Ocean ⓘ
length approximately 17.6 m ⓘ
manufacturer Northrop Grumman Innovation Systems ⓘ
linked to: Northrop Grumman

Orbital Sciences Corporation ⓘ
marketSegment small satellite launch ⓘ
notableFeature dropped from carrier aircraft before ignition ⓘ
winged first stage for atmospheric flight ⓘ
numberOfStages 3 ⓘ
operator Northrop Grumman Space Systems ⓘ
Orbital ATK ⓘ
Orbital Sciences Corporation ⓘ
primaryUse launch of scientific spacecraft ⓘ
launch of small satellites ⓘ
launch of technology demonstration payloads ⓘ
propellantType solid fuel ⓘ
secondStageName Orion 50XL ⓘ
linked to: Orion 50SXL
stagesConfiguration three-stage solid rocket ⓘ
stageSeparation sequential solid-stage separation ⓘ
status operational ⓘ
successorTo Pegasus ⓘ
thirdStageName Orion 38 ⓘ
typicalInclinations equatorial or mid-inclination LEO ⓘ
typicalPayloadMassToLEO approximately 443 kg ⓘ

How these facts were elicited

Referenced by (16)

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

SCISAT-1 → launchVehicle → Pegasus XL ⓘ
NuSTAR → launchVehicle → Pegasus XL ⓘ
GALEX → launchVehicle → Pegasus XL ⓘ
subject linked to: GALEX Galaxy Evolution Explorer
Orbital Sciences Corporation → notableProduct → Pegasus air-launched rocket ⓘ
linked to: Pegasus XL
MAESTRO → launchVehicle → Pegasus XL ⓘ
Orion 50SXL → usedOnVehicle → Pegasus XL ⓘ
Orion 38 → usedOn → Pegasus XL ⓘ
Pegasus rocket family → familyMember → Pegasus H ⓘ
linked to: Pegasus XL
Stargazer → launchVehicleCarried → Pegasus XL ⓘ
ICON → launchVehicle → Pegasus XL ⓘ