Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
fighter aircraft
|
| gptkbp:aircraft |
reconnaissance
advanced materials high agility interceptor ground attack high thrust-to-weight ratio advanced flight control system tailless delta wing low observable technology stealth fighter empty weight 18,000 kg maximum takeoff weight 30,000 kg |
| gptkbp:armament |
cannon
air-to-air missiles air-to-ground missiles |
| gptkbp:avionics |
digital fly-by-wire system
|
| gptkbp:cockpit |
glass cockpit
|
| gptkbp:countermeasures |
electronic warfare system
|
| gptkbp:crew |
gptkb:Mikhail_Gromov
|
| gptkbp:design |
stealth_technology
|
| gptkbp:design_feature |
supercruise capability
canard_wings |
| gptkbp:engineType |
twin-engine
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuel_capacity |
5,000 liters
|
| gptkbp:hasExperienceIn |
1,500 km
|
| gptkbp:height |
4.8 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mikoyan MiG-1.44
|
| gptkbp:inspiration |
gptkb:Mikoyan_MiG-31
gptkb:Mikoyan_MiG-29 network-centric warfare advanced avionics high maneuverability |
| gptkbp:inventor |
1
|
| gptkbp:landing_gear |
retractable landing gear
|
| gptkbp:length |
20.2 m
|
| gptkbp:manufacturer |
gptkb:Mikoyan
|
| gptkbp:maximum_speed |
Mach_2.5
|
| gptkbp:maxTakeoffWeight |
25,000 kg
|
| gptkbp:operational_status |
cancelled
|
| gptkbp:origin |
gptkb:Russia
|
| gptkbp:productionYears |
1990s to early 2000s
|
| gptkbp:project |
1990
2005 |
| gptkbp:radar |
phased array radar
|
| gptkbp:role |
air superiority fighter
|
| gptkbp:safety_features |
reduced radar cross-section
|
| gptkbp:service_ceiling |
20,000 m
|
| gptkbp:successor |
gptkb:Mikoyan_MiG-35
|
| gptkbp:targets |
infrared search and track
|
| gptkbp:team |
gptkb:Mikoyan_design_bureau
multirole fighter |
| gptkbp:wingspan |
14.5 m
|