Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:afterburnerThrust |
29,160 lbf (129.7 kN)
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.36:1
|
| gptkbp:compressionRatio |
25:1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
two-spool axial-flow
|
| gptkbp:diameter |
34.8 in (0.88 m)
|
| gptkbp:firstFlight |
1972
|
| gptkbp:fuelType |
gptkb:JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F100-PW-100
|
| gptkbp:length |
191 in (4.85 m)
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:relatedModel |
gptkb:Pratt_&_Whitney_F100-PW-229
gptkb:Pratt_&_Whitney_F100-PW-220 Pratt & Whitney F100-PW-200 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
23,830 lbf (106.0 kN)
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:General_Dynamics_F-16_Fighting_Falcon
gptkb:McDonnell_Douglas_F-15_Eagle |
| gptkbp:weight |
3,800 lb (1,724 kg)
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_F100-PW-220
|
| gptkbp:bfsLayer |
7
|