Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.58:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
14-stage axial
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
43 in
|
| gptkbp:family |
gptkb:Rolls-Royce_Spey
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
aviation kerosene
|
| gptkbp:hasTower |
2-stage high pressure, 2-stage low pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
Spey Mk.101
|
| gptkbp:length |
146 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
20,515 lbf
|
| gptkbp:usedBy |
gptkb:Royal_Air_Force
gptkb:Royal_Navy |
| gptkbp:usedIn |
gptkb:McDonnell_Douglas_F-4_Phantom_II
|
| gptkbp:weight |
3,900 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Spey
|
| gptkbp:bfsLayer |
7
|