Statements (90)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:F135-PW-100_Engine
|
| gptkbp:aircraft_operated |
gptkb:F-22_Raptor
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
FAA certified
military certification |
| gptkbp:check_in_time |
gptkb:battle
|
| gptkbp:compression_ratio |
30:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system |
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:developer |
gptkb:Joint_Strike_Fighter_program
1990s |
| gptkbp:diameter |
3.0 ft
3.5 ft 3 ft 4 in |
| gptkbp:emissions_standard |
low
low emissions |
| gptkbp:engine |
gptkb:aircraft
performance metrics high availability high performance modular design technological advancements state-of-the-art technology high reliability twin-engine advanced features innovative design twin-spool ongoing development developed in the 1990s ongoing research and development global support network air start advanced design supercruise capability influenced future engine designs advanced materials used detailed specifications collaboration with military partners 35,000 lbf 26,000 lbf without afterburner upgradable for future needs |
| gptkbp:engine_type |
axial compressor
dual-spool high bypass turbofan military turbofan |
| gptkbp:fan_art |
wide-chord fan
|
| gptkbp:features |
supercruise capability
vectoring thrust |
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_capacity |
high
3.5 ft 3,000 lb 0.5 lb/hp/hr 0.5 lb/lbf/hr 16.5 ft 5.03 m 816 kg 1.02 m superior capabilities |
| gptkbp:fuel_type |
gptkb:JP-8
annular combustor |
| https://www.w3.org/2000/01/rdf-schema#label |
F119-PW-100 engine
|
| gptkbp:is_tested_for |
extensive testing
extensive ground testing |
| gptkbp:length |
16 ft 6 in
16.5 ft |
| gptkbp:maintenance |
long
1,000 hours |
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:max_speed |
Mach 2.25
|
| gptkbp:noise_level |
low
low noise |
| gptkbp:operational_range |
long
|
| gptkbp:operational_status |
in service
|
| gptkbp:power_output |
29,000 lbf
|
| gptkbp:propulsion |
gptkb:battle
35,000 lbf 2 D thrust vectoring |
| gptkbp:reliability |
high
|
| gptkbp:service_ceiling |
65,000 ft
|
| gptkbp:services |
gptkb:2005
|
| gptkbp:supports |
3,000 lb/s
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Lockheed_Martin_F-22_Raptor
|
| gptkbp:weight |
1,800 lb
3,000 lb |