Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.58:1
|
| gptkbp:compressionRatio |
two-spool axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
43 in
|
| gptkbp:family |
gptkb:Rolls-Royce_Spey
|
| gptkbp:firstFlight |
1966
|
| https://www.w3.org/2000/01/rdf-schema#label |
Spey Mk.512
|
| gptkbp:length |
146 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:status |
out of production
|
| gptkbp:thrust |
yes
20,515 lbf |
| gptkbp:usedIn |
gptkb:McDonnell_Douglas_F-4K_Phantom_II
gptkb:McDonnell_Douglas_F-4M_Phantom_II |
| gptkbp:weight |
3,820 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_Spey
|
| gptkbp:bfsLayer |
7
|