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 (2)

Label Occurrences
Pegasus XL canonical 5
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 of America
surface form: 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 Lockheed L-1011 TriStar
surface form: Stargazer L-1011
launchServiceProvider Northrop Grumman
Orbital Sciences Corporation
surface form: 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
surface form: Northrop Grumman Innovation Systems

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 Technology
surface form: Northrop Grumman Space Systems

Orbital Sciences Corporation
surface form: Orbital ATK

Orbital Sciences Corporation
primaryUse launch of scientific spacecraft
launch of small satellites
launch of technology demonstration payloads
propellantType solid fuel
secondStageName Orion 50SXL
surface form: Orion 50XL
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 (6)

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

SCISAT-1 launchVehicle Pegasus XL
NuSTAR Nuclear Spectroscopic Telescope Array launchVehicle Pegasus XL
subject surface form: NuSTAR
GALEX Galaxy Evolution Explorer launchVehicle Pegasus XL
subject surface form: GALEX
Orbital Sciences Corporation notableProduct Pegasus XL
this entity surface form: Pegasus air-launched rocket
MAESTRO launchVehicle Pegasus XL