Properties (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
gptkb:F-16
gptkb:F-15 |
| gptkbp:controls |
FADEC
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engine |
low noise
air start pylon-mounted |
| gptkbp:engineConfiguration |
twin-engine
|
| gptkbp:engineType |
axial compressor
F100-PW-100 F100-PW-220 F100-PW-229 axial turbine F100-PW-229E F100-PW-229E-220 F100-PW-229E-229 F100-PW-229E-229E F100-PW-229E-229E-220 F100-PW-229E-229E-229 |
| gptkbp:firstFlight |
1976
|
| gptkbp:firstHeld |
gptkb:F-15_Eagle
F-16 Fighting Falcon |
| gptkbp:fuel_capacity |
1,200 lb/hr
|
| gptkbp:fuelType |
JP-8
annular combustor |
| gptkbp:hasContent |
0.8 lb/lbf/hr
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F100
|
| gptkbp:length |
3.8 m
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:maxSpeed |
Mach_2.5
|
| gptkbp:notableFeature |
afterburner
digital engine control variable geometry inlet |
| gptkbp:operationalStatus |
in service
1,500 °F |
| gptkbp:performances |
4,000 hours
|
| gptkbp:propulsion |
24:1
up to 29,000 lbf |
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:services |
50,000 ft
|
| gptkbp:successor |
Pratt & Whitney F119
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:F-15_Eagle
F-16 Fighting Falcon |
| gptkbp:weight |
1,200 kg
|