|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:application
|
air launch to orbit
|
|
gptkbp:book
|
Orion 50
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
1.27 m
|
|
gptkbp:firstFlight
|
1990-04-05
|
|
gptkbp:firstOrbitalLaunch
|
gptkb:Pegasus_(original)
|
|
gptkbp:launchSite
|
air-launched from aircraft
|
|
gptkbp:launchVehicle
|
gptkb:satellite
gptkb:air-launched_rocket
|
|
gptkbp:length
|
16.9 m (Pegasus XL)
|
|
gptkbp:manufacturer
|
gptkb:Orbital_Sciences_Corporation
|
|
gptkbp:mass
|
23,130 kg (Pegasus XL)
|
|
gptkbp:notableMission
|
gptkb:HETE-2
gptkb:IRIS
gptkb:NuSTAR
AeroCube
|
|
gptkbp:notableVariant
|
gptkb:Pegasus-H
gptkb:Pegasus_XL
Pegasus-FT
|
|
gptkbp:numberOfStages
|
3
Orion 50S
|
|
gptkbp:operator
|
gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:payloadToLEO
|
443 kg
|
|
gptkbp:platform
|
Lockheed L-1011 Stargazer
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:status
|
active
|
|
gptkbp:thirdStageEngine
|
gptkb:Orion_38
|
|
gptkbp:usedFor
|
launching small satellites
|
|
gptkbp:website
|
https://www.northropgrumman.com/space/pegasus-rocket/
|
|
gptkbp:bfsParent
|
gptkb:Taurus_rocket
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pegasus rocket family
|