Statements (24)
| 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 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_F100
|
| gptkbp:features |
improved reliability
increased thrust digital electronic engine control |
| gptkbp:firstFlight |
1989
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F100-PW-229
|
| gptkbp:improves |
gptkb:Pratt_&_Whitney_F100-PW-220
|
| gptkbp:length |
191 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
17,800 lbf
|
| gptkbp:thrustAfterburner |
29,160 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:F-16C/D_Fighting_Falcon
F-15E Strike Eagle |
| gptkbp:weight |
3,875 lb
|
| gptkbp:bfsParent |
gptkb:F-16V_Viper
|
| gptkbp:bfsLayer |
5
|