Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
34.8 in
|
| gptkbp:firstFlight |
1970
|
| gptkbp:fuelType |
gptkb:JP-8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F100
|
| gptkbp:introduced |
1974
|
| gptkbp:length |
191 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notableFeature |
modular design
digital electronic engine control (DEEC) in later variants |
| gptkbp:numberOfStages |
2-stage HP, 2-stage LP
3-stage fan, 10-stage HP compressor |
| gptkbp:status |
in service
|
| gptkbp:thrust |
29,000 lbf
17,800 lbf |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:aircraft
F-15 Eagle |
| gptkbp:variant |
gptkb:F100-PW-100
gptkb:F100-PW-200 gptkb:F100-PW-220 gptkb:F100-PW-229 |
| gptkbp:weight |
3,920 lb
|
| gptkbp:bfsParent |
gptkb:F-16V_Fighting_Falcon
gptkb:Pratt_&_Whitney_F100-PW-229 gptkb:F-16 gptkb:General_Dynamics_F-16_Fighting_Falcon gptkb:General_Dynamics_F-16 gptkb:F-16_ברק |
| gptkbp:bfsLayer |
6
|