Statements (52)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:aircraft
|
gptkbp:air_traffic_control |
demonstrate technology for future use
|
gptkbp:aircraft_configuration |
single-engine configuration
aerodynamically optimized |
gptkbp:aircraft_operated |
state-of-the-art technology
advanced avionics highly efficient supersonic aircraft approximately 30,000 pounds new flight technologies capable of supersonic speeds |
gptkbp:aircraft_role |
gptkb:aircraft
|
gptkbp:aircraft_type |
experimental supersonic aircraft
|
gptkbp:cockpit |
single-seat cockpit
|
gptkbp:collaboration |
NASA and Lockheed Martin
|
gptkbp:control_system |
fly-by-wire
|
gptkbp:crew |
1 pilot
|
gptkbp:design |
quiet supersonic technology
|
gptkbp:design_feature |
low boom design
|
gptkbp:engine_type |
gptkb:General_Electric_F414
|
gptkbp:environmental_impact |
reduced sonic booms
|
gptkbp:first_flight |
gptkb:2022
initial flight tests conducted in the 2020s focused on noise reduction |
gptkbp:flight_style |
expanded supersonic flight envelope
|
gptkbp:fuel_capacity |
approximately 10,000 pounds
|
gptkbp:funding |
gptkb:NASA
|
gptkbp:has_programs |
gptkb:NASA's_Low_Boom_Flight_Demonstrator
|
https://www.w3.org/2000/01/rdf-schema#label |
X-59 Que S59 T
|
gptkbp:impact |
potential for commercial supersonic flights
|
gptkbp:is_tested_for |
gptkb:NASA_Armstrong_Flight_Research_Center
inform regulatory standards |
gptkbp:length |
94 feet
|
gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
gptkbp:max_speed |
Mach 1.4
|
gptkbp:mission |
gather data on public perception
|
gptkbp:noise_level |
below 75 perceived decibels
|
gptkbp:notable_project |
advancing supersonic travel
|
gptkbp:partnership |
government and industry collaboration
|
gptkbp:project |
multi-year project
demonstrate low boom technology |
gptkbp:projected_operational_use |
commercial aviation
|
gptkbp:purpose |
supersonic flight testing
|
gptkbp:research_focus |
supersonic flight over land
|
gptkbp:research_output |
data for future supersonic designs
|
gptkbp:status |
in development
|
gptkbp:target_noise_reduction |
community acceptance
|
gptkbp:test_flight_objectives |
assess community response to noise
|
gptkbp:wing_configuration |
delta wing
|
gptkbp:wingspan |
29.5 feet
|
gptkbp:year |
2025
|