Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.36:1
|
| gptkbp:compressionRatio |
25:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
34.8 in (0.88 m)
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_F100
|
| gptkbp:firstFlight |
1989
|
| https://www.w3.org/2000/01/rdf-schema#label |
F100-PW-229
|
| gptkbp:length |
191 in (4.85 m)
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:operator |
gptkb:Royal_Netherlands_Air_Force
gptkb:Royal_Norwegian_Air_Force gptkb:United_States_Air_Force gptkb:Republic_of_Korea_Air_Force gptkb:Royal_Danish_Air_Force gptkb:Israeli_Air_Force gptkb:Egyptian_Air_Force gptkb:Royal_Saudi_Air_Force gptkb:Singapore_Air_Force |
| gptkbp:status |
in service
|
| gptkbp:thrust |
17,800 lbf (military power)
29,160 lbf (afterburner) |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
F-15 Eagle |
| gptkbp:weight |
3,875 lb (1,757 kg)
|
| gptkbp:bfsParent |
gptkb:F100
gptkb:Pratt_&_Whitney_F100 |
| gptkbp:bfsLayer |
7
|