Statements (138)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:air_traffic_control |
demonstrate low-boom technology to regulators
|
| gptkbp:aircraft_configuration |
single-engine design
optimized for low boom |
| gptkbp:aircraft_operated |
gptkb:aircraft
approximately 1 hour advanced aerodynamics 40,000 pounds highly efficient ongoing development approximately 30,000 pounds experimental aircraft category above 50,000 feet experimental supersonic aircraft unique aerodynamic design NX-59 A highly efficient flight |
| gptkbp:aircraft_role |
gptkb:aircraft
|
| gptkbp:aircraft_testing_phase |
flight demonstration phase
|
| gptkbp:aircraft_type |
fixed-wing aircraft
supersonic aircraft |
| gptkbp:application |
commercial supersonic travel
|
| gptkbp:avionics |
advanced avionics suite
|
| gptkbp:cancellation_reason |
shaping and materials
|
| gptkbp:clinical_trial |
several years
|
| gptkbp:cockpit |
glass cockpit
single-pilot cockpit |
| gptkbp:collaboration |
Lockheed Martin and NASA
partnerships with global aviation agencies |
| gptkbp:collaborations |
collaborations with universities
government and industry partners NASA and industry partners |
| gptkbp:collaborator |
gptkb:US_Air_Force
gptkb:Lockheed_Martin_Skunk_Works |
| gptkbp:collection |
sonic boom data collection
|
| gptkbp:community_engagement |
public outreach programs
|
| gptkbp:community_outreach |
gptkb:public_engagement_initiatives
|
| gptkbp:control_surfaces |
elevons
canards |
| gptkbp:control_system |
fly-by-wire
fly-by-wire system |
| gptkbp:crew |
1 pilot
|
| gptkbp:design |
gptkb:Lockheed_Martin_Skunk_Works
completed final design phase Lockheed Martin engineers |
| gptkbp:design_feature |
long fuselage
|
| gptkbp:design_purpose |
quiet supersonic travel
quiet supersonic flight |
| gptkbp:designed_by |
gptkb:NASA
|
| gptkbp:designed_for |
low-boom supersonic travel
|
| gptkbp:development_cost |
$247 million
|
| gptkbp:elevation |
60,000 feet
|
| gptkbp:engine_type |
gptkb:F414
gptkb:F414_engine |
| gptkbp:environmental_impact |
reduced noise pollution
|
| gptkbp:first_flight |
gptkb:Michael_
gptkb:2022 gptkb:California ongoing data for future designs various locations in the U. S. demonstrate low boom capabilities initial flight tests demonstrating low-boom technology real-world flight conditions validate performance metrics |
| gptkbp:flight_style |
subsonic and supersonic
|
| gptkbp:flight_test_duration |
up to 3 hours
|
| gptkbp:flight_test_goals |
data collection for regulatory approval
|
| gptkbp:flight_test_program |
gptkb:NASA's_Supersonic_Transport_Program
|
| gptkbp:flight_testing_goal |
validate low-boom design
|
| gptkbp:fuel_capacity |
14,000 pounds
|
| gptkbp:funding |
gptkb:NASA
government funding |
| gptkbp:fuselage_material |
composite materials
|
| gptkbp:goal |
to reduce sonic boom noise
reduce sonic boom noise |
| gptkbp:has_programs |
gptkb:Low_Boom_Flight_Demonstration
gptkb:NASA's_Low_Boom_Flight_Demonstrator |
| gptkbp:height |
14.5 feet
|
| https://www.w3.org/2000/01/rdf-schema#label |
X-59 Que SST
|
| gptkbp:is_a_supporter_of |
planned for future events
|
| gptkbp:is_funded_by |
gptkb:U._S._government
|
| gptkbp:is_tested_for |
gptkb:NASA_Armstrong_Flight_Research_Center
flight tests flight testing data for future supersonic designs |
| gptkbp:landing_gear |
tricycle landing gear
retractable landing gear |
| gptkbp:length |
94 feet
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:max_speed |
Mach 1.4
|
| gptkbp:max_takeoff_weight |
55,000 pounds
|
| gptkbp:mission |
evaluate low boom technology
sonic boom reduction evaluate performance and noise levels |
| gptkbp:noise_level |
community feedback
low sonic boom below 75 perceived decibels |
| gptkbp:notable_pilots |
gptkb:NASA_test_pilots
|
| gptkbp:number_of_engines |
gptkb:1
|
| gptkbp:operational_range |
1,500 nautical miles
|
| gptkbp:operational_use |
commercial supersonic flights
|
| gptkbp:outcome |
new regulations for supersonic flight
|
| gptkbp:partnership |
NASA and Lockheed Martin
|
| gptkbp:project |
managed by NASA
multi-year project NASA and Lockheed Martin commercial viability of supersonic travel |
| gptkbp:public_interest |
high public interest in supersonic travel
|
| gptkbp:purpose |
supersonic flight research
supersonic flight testing |
| gptkbp:range |
2,500 nautical miles
|
| gptkbp:regulatory_compliance |
influence future supersonic regulations
|
| gptkbp:research_focus |
sonic boom perception
public acceptance of supersonic travel civilian supersonic travel |
| gptkbp:roll_rate |
5 degrees per second
|
| gptkbp:safety_features |
redundant systems
|
| gptkbp:service_entry |
2025
|
| gptkbp:speed |
Mach 1.4
|
| gptkbp:stall_speed |
120 knots
|
| gptkbp:status |
in development
|
| gptkbp:sustainability |
environmentally friendly design
|
| gptkbp:target_audience |
civil aviation industry
|
| gptkbp:test_flight_frequency |
multiple flights per month
|
| gptkbp:test_flight_schedule |
2022-2025
|
| gptkbp:test_flights_location |
gptkb:NASA_Armstrong_Flight_Research_Center
|
| gptkbp:wing_configuration |
delta wing
|
| gptkbp:wingspan |
29.5 feet
94.5 feet |
| gptkbp:year |
gptkb:2016
gptkb:2018 gptkb:2023 2025 |
| gptkbp:bfsParent |
gptkb:NASA
|
| gptkbp:bfsLayer |
3
|