Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:ChineseLicense |
WS-9
|
| gptkbp:civilVariant |
Spey 511
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_RB.163
|
| gptkbp:diameter |
1.04 m
|
| gptkbp:firstRun |
1954
|
| https://www.w3.org/2000/01/rdf-schema#label |
Spey engine
|
| gptkbp:length |
2.51 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:militaryBranch |
gptkb:Spey_Mk.101
gptkb:Spey_Mk.202 gptkb:Spey_Mk.250 Spey Mk.203 |
| gptkbp:notableFeature |
compact design
high reliability |
| gptkbp:notableUser |
gptkb:Royal_Air_Force
gptkb:Royal_Navy China (licensed production) |
| gptkbp:successor |
gptkb:Rolls-Royce_Tay
|
| gptkbp:thrust |
10,000–12,000 lbf
|
| gptkbp:type |
low-bypass turbofan
|
| gptkbp:usedInAircraft |
gptkb:BAC_One-Eleven
gptkb:Blackburn_Buccaneer gptkb:Hawker_Siddeley_Nimrod gptkb:Grumman_Gulfstream_II F-4 Phantom II (British variants) |
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Tay_611-8
|
| gptkbp:bfsLayer |
7
|