Statements (137)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:aircraft
|
gptkbp:bfsLayer |
3
|
gptkbp:bfsParent |
gptkb:NASA
|
gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:NASA_test_pilots approximately 1 hour advanced aerodynamics fixed-wing aircraft 40,000 pounds highly efficient supersonic aircraft delta wing ongoing development approximately 30,000 pounds experimental aircraft category above 50,000 feet experimental supersonic aircraft single-engine design unique aerodynamic design NX-59 A demonstrate low-boom technology to regulators flight demonstration phase highly efficient flight optimized for low boom |
gptkbp:airlines |
gptkb:NASA_Armstrong_Flight_Research_Center
|
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:collaborations |
gptkb:US_Air_Force
gptkb:Lockheed_Martin_Skunk_Works collaborations with universities government and industry partners Lockheed Martin and NASA partnerships with global aviation agencies NASA and industry partners |
gptkbp:collection |
sonic boom data collection
|
gptkbp:community_engagement |
public outreach programs
high public interest in supersonic travel |
gptkbp:community_involvement |
gptkb:public_engagement_initiatives
|
gptkbp:controls |
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 quiet supersonic travel quiet supersonic flight |
gptkbp:designed_by |
gptkb:NASA
|
gptkbp:developer |
$247 million
|
gptkbp:elevation |
60,000 feet
|
gptkbp:engine |
gptkb:musical
|
gptkbp:engine_type |
gptkb:F414
gptkb:F414_engine |
gptkbp:environmental_impact |
reduced noise pollution
|
gptkbp:features |
long fuselage
|
gptkbp:first_flight |
gptkb:NASA's_Supersonic_Transport_Program
gptkb:Michael_ gptkb:2022 gptkb:California ongoing up to 3 hours 2022-2025 subsonic and supersonic data for future designs various locations in the U. S. demonstrate low boom capabilities initial flight tests data collection for regulatory approval demonstrating low-boom technology real-world flight conditions validate low-boom design validate performance metrics |
gptkbp:frequency |
multiple flights per month
|
gptkbp:fuel_capacity |
14,000 pounds
|
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_designed_for |
low-boom supersonic travel
|
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:material |
composite materials
|
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:operational_range |
1,500 nautical miles
|
gptkbp:operational_status |
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:purpose |
supersonic flight research
supersonic flight testing |
gptkbp:range |
2,500 nautical miles
|
gptkbp:receives_funding_from |
gptkb:U._S._government
gptkb:NASA government funding |
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:services |
2025
|
gptkbp:speed |
120 knots
Mach 1.4 |
gptkbp:status |
in development
|
gptkbp:surface |
elevons
canards |
gptkbp:sustainability |
environmentally friendly design
|
gptkbp:target_audience |
civil aviation industry
|
gptkbp:wingspan |
29.5 feet
94.5 feet |
gptkbp:year |
gptkb:2016
gptkb:2018 gptkb:2023 2025 |