Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:afterburnerThrust |
25,000 lbf
|
| gptkbp:bypassRatio |
0.36:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
3-stage fan, 10-stage HP compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
34.8 in
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_F100
|
| gptkbp:firstFlight |
1972
|
| gptkbp:hasTower |
2-stage HP, 2-stage LP
|
| gptkbp:length |
191 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:militaryDesignation |
gptkb:F100-PW-100
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:F100-PW-220
|
| gptkbp:thrust |
23,830 lbf
|
| gptkbp:usedIn |
gptkb:aircraft
F-15 Eagle |
| gptkbp:weight |
3,800 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_F100_turbofan
gptkb:F100 gptkb:General_Electric_F100_family gptkb:Pratt_&_Whitney_F100 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
F100-PW-100
|