Rolls-Royce AE 3007H
E558712
The Rolls-Royce AE 3007H is a high-bypass turbofan engine variant developed by Rolls-Royce to power high-altitude, long-endurance unmanned aerial vehicles such as the RQ-4 Global Hawk.
Statements (30)
| Predicate | Object |
|---|---|
| instanceOf | turbofan engine ⓘ |
| basedOn | Rolls-Royce AE 3007 civil engine core ⓘ |
| bypassRatio | high-bypass ⓘ |
| certificationUse | military application ⓘ |
| configuration | two-spool ⓘ |
| countryOfOrigin | United Kingdom ⓘ |
| designGoal |
fuel efficiency at high altitude
ⓘ
long-endurance operation ⓘ reliability for unmanned operations ⓘ |
| developedFor | high-altitude long-endurance unmanned aerial vehicles ⓘ |
| developer | Rolls-Royce North America NERFINISHED ⓘ |
| familyApplication |
business jets
ⓘ
regional jets ⓘ |
| feature |
FADEC control
ⓘ
single engine installation on Global Hawk ⓘ |
| intendedEnvironment |
high-altitude flight
ⓘ
long-endurance missions ⓘ |
| manufacturer | Rolls-Royce NERFINISHED ⓘ |
| notableCharacteristic |
derivative of a commercial engine family
ⓘ
optimized for unmanned operation ⓘ |
| partOfFamily | Rolls-Royce AE 3007 NERFINISHED ⓘ |
| primaryApplication |
MQ-4C Triton
NERFINISHED
ⓘ
Northrop Grumman RQ-4 Global Hawk NERFINISHED ⓘ |
| role | propulsion for ISR UAVs ⓘ |
| thrustClass | approximately 7,000–8,000 lbf ⓘ |
| usedBy |
United States Air Force
ⓘ
United States Navy ⓘ |
| usedOnAircraft |
MQ-4C Triton
NERFINISHED
ⓘ
RQ-4 Global Hawk NERFINISHED ⓘ |
| usedOnAircraftType | unmanned aerial vehicle ⓘ |
Referenced by (2)
Full triples — surface form annotated when it differs from this entity's canonical label.