Orion 38

E824041

Orion 38 is a solid-fueled upper-stage rocket motor used as the third stage on certain Pegasus XL launch vehicles to deliver payloads into orbit.

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Statements (48)

Predicate Object
instanceOf rocket stage
solid-fueled rocket motor
upper stage
application commercial launches
government launches
scientific missions
attitudeControl spin-stabilized
burnMode single-burn
burnTime approximately 68 s
caseMaterial composite material
countryOfOrigin United States of America
surface form: United States
designLife single use
developedFor small satellite launches
diameter 0.97 m
environmentOfOperation vacuum
family Orion rocket motor family NERFINISHED
fuelGrainGeometry internal burning grain
ignitionType pyrotechnic ignition
launchVehicleRole orbital insertion stage
launchVehicleType air-launched launch vehicle
length 2.34 m
manufacturer Northrop Grumman Innovation Systems NERFINISHED
Orbital Sciences Corporation NERFINISHED
missionType LEO missions
SSO missions
natoName Orion-38 NERFINISHED
nozzleType fixed nozzle
operatedBy Northrop Grumman NERFINISHED
Orbital ATK NERFINISHED
Orbital Sciences Corporation NERFINISHED
propellantMass approximately 770 kg
propellantType solid propellant
separationSystem used with interstage adapter
specificImpulseVacuum approximately 294 s
stageNumberOnPegasusXL 3
staging solid rocket stage
status operational
thrustVectorControl none
totalMass approximately 873 kg
usedAs third stage
usedFor placing payloads into orbit
usedIn expendable launch systems
usedOn Pegasus NERFINISHED
Pegasus XL NERFINISHED
Pegasus XL HAPS configurations
usedSince 1990s
usedWith Pegasus XL payload fairing NERFINISHED
vacuumThrust approximately 32 kN

Referenced by (1)

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

Pegasus XL thirdStageName Orion 38