Pratt & Whitney F100-PW-229
GPTKB entity
Properties (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
jet engine
|
| gptkbp:aircraft |
F-15_and_F-16
|
| gptkbp:controls |
digital electronic control
|
| gptkbp:coolingSystem |
advanced cooling techniques
|
| gptkbp:diameter |
36 inches
|
| gptkbp:engine |
military aircraft
state-of-the-art design |
| gptkbp:engineConfiguration |
twin-spool
ongoing production |
| gptkbp:engineType |
turbofan
advanced materials axial high bypass ratio F100-PW-220, F100-PW-229 |
| gptkbp:firstFlight |
1986
|
| gptkbp:fuelType |
annular
JP-8 |
| gptkbp:hasArea |
extensive testing program
FAA_certification_not_applicable |
| gptkbp:hasExperienceIn |
over 2,000 miles
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney F100-PW-229
|
| gptkbp:is_used_in |
gptkb:F-15_Eagle
F-16 Fighting Falcon |
| gptkbp:length |
156 inches
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:militaryRank |
none
F100-PW-229 |
| gptkbp:noise_level |
yes
|
| gptkbp:notable_feature |
reduced radar cross-section
|
| gptkbp:operational_status |
air superiority missions
|
| gptkbp:operationalRange |
high performance
|
| gptkbp:performances |
modular design
high reliability high efficiency high thrust-to-weight ratio detailed specifications available. |
| gptkbp:primaryUser |
gptkb:United_States_Air_Force
|
| gptkbp:propulsion |
optional
29,000 lbf 32,000 lbf 9.67 |
| gptkbp:related_engine |
F100 family
Brayton_cycle |
| gptkbp:reviews |
29,000 lbf to 32,000 lbf
|
| gptkbp:serviceHistory |
in service since 1986
|
| gptkbp:training |
F100 development program
|
| gptkbp:type |
afterburning turbofan engine
|
| gptkbp:updates |
available upgrades
|
| gptkbp:variant |
F100 engine family
|
| gptkbp:weight |
3,000 lb
|