Rolls-Royce AE 3007H turbofan
GPTKB entity
Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
unmanned aerial vehicles
|
| gptkbp:bypassRatio |
5:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
14-stage axial
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
0.965 m
|
| gptkbp:family |
gptkb:Rolls-Royce_AE_3007
|
| gptkbp:firstFlight |
1998
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
2-stage high pressure, 3-stage low pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 3007H turbofan
|
| gptkbp:length |
2.3 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
7,050 lbf
|
| gptkbp:usedIn |
gptkb:Northrop_Grumman_RQ-4_Global_Hawk
gptkb:MQ-4C_Triton |
| gptkbp:weight |
637 kg
|
| gptkbp:bfsParent |
gptkb:RQ-4A
gptkb:MQ-4C gptkb:Northrop_Grumman_MQ-4C_Triton |
| gptkbp:bfsLayer |
7
|