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.

All labels observed (2)

Label Occurrences
Orion 38 canonical 1
Orion-38 1

How this entity was disambiguated

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 ⓘ
designLife single use ⓘ
developedFor small satellite launches ⓘ
diameter 0.97 m ⓘ
environmentOfOperation vacuum ⓘ
family Orion rocket motor family ⓘ
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 ⓘ
linked to: Northrop Grumman

Orbital Sciences Corporation ⓘ
missionType LEO missions ⓘ
SSO missions ⓘ
natoName Orion-38 ⓘ
linked to: Orion 38
nozzleType fixed nozzle ⓘ
operatedBy Northrop Grumman ⓘ
Orbital ATK ⓘ
Orbital Sciences Corporation ⓘ
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 ⓘ
Pegasus XL ⓘ
Pegasus XL HAPS configurations ⓘ
usedSince 1990s ⓘ
usedWith Pegasus XL payload fairing ⓘ
vacuumThrust approximately 32 kN ⓘ

How these facts were elicited

Referenced by (2)

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

Pegasus XL → thirdStageName → Orion 38 ⓘ
Orion 38 → natoName → Orion-38 ⓘ
linked to: Orion 38