Statements (65)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:air_traffic_control |
digital flight control system
|
| gptkbp:aircraft_configuration |
variable geometry
asymmetric configuration |
| gptkbp:aircraft_operated |
enhanced aircraft performance
advanced aerodynamic features over 200 flight hours |
| gptkbp:aircraft_program |
gptkb:X-29_program
|
| gptkbp:aircraft_type |
gptkb:fighter_aircraft
|
| gptkbp:avionics |
advanced avionics system
|
| gptkbp:collaborations |
collaboration with universities
|
| gptkbp:conducts_research_on |
aerodynamics
|
| gptkbp:control_surfaces |
variable camber control surfaces
|
| gptkbp:control_system |
fly-by-wire
|
| gptkbp:crew |
gptkb:1
|
| gptkbp:design |
Mc Donnell Douglas design team
|
| gptkbp:design_date |
gptkb:1976
|
| gptkbp:design_feature |
forward-swept wings
|
| gptkbp:design_philosophy |
innovative design philosophy
|
| gptkbp:elevation |
15,000 m
|
| gptkbp:engine_type |
twin-engine
|
| gptkbp:first_flight |
gptkb:1984
extensive flight testing numerous test flights collected extensive flight data evaluation of flight characteristics multiple flight testing phases |
| gptkbp:flight_style |
expanded flight envelope
unique flight characteristics |
| gptkbp:funding |
funded by U. S. government
|
| gptkbp:fuselage_material |
composite materials
|
| gptkbp:has_authority_over |
enhanced control authority
increased control authority |
| https://www.w3.org/2000/01/rdf-schema#label |
X-29 aircraft
|
| gptkbp:impact |
significant impact on aerospace research
|
| gptkbp:influence |
future aircraft designs
|
| gptkbp:invention |
2
|
| gptkbp:is_tested_for |
gptkb:NASA
|
| gptkbp:landing_gear |
tricycle landing gear
|
| gptkbp:legacy |
influenced modern aircraft technology
|
| gptkbp:length |
15.2 m
|
| gptkbp:manufacturer |
gptkb:Mc_Donnell_Douglas
|
| gptkbp:max_speed |
Mach 2.5
|
| gptkbp:mission |
demonstrate advanced technologies
|
| gptkbp:notable_battle |
high maneuverability
|
| gptkbp:notable_pilots |
gptkb:NASA_test_pilots
gptkb:training |
| gptkbp:operational_history |
1984 to 1996
|
| gptkbp:project |
12 years
completed in 1996 |
| gptkbp:research_areas |
flight dynamics
|
| gptkbp:research_focus |
control surfaces
|
| gptkbp:research_institutes |
gptkb:NASA_Ames_Research_Center
|
| gptkbp:research_output |
data for future aircraft
|
| gptkbp:retirement_year |
gptkb:1996
|
| gptkbp:role |
technology demonstrator
|
| gptkbp:roll_rate |
high roll rate
active roll control system |
| gptkbp:significance |
advanced flight technologies
|
| gptkbp:stall_speed |
improved stall characteristics
|
| gptkbp:stealth_features |
limited radar cross-section
|
| gptkbp:wind_tunnel_testing |
wind tunnel testing conducted
|
| gptkbp:wingspan |
11.6 m
|
| gptkbp:bfsParent |
gptkb:Skunk_Works_X-44
|
| gptkbp:bfsLayer |
6
|