|
gptkbp:instance_of
|
gptkb:aircraft
gptkb:Team_Rocket
|
|
gptkbp:aircraft_configuration
|
gptkb:monoplane
single-engine
|
|
gptkbp:aircraft_operated
|
breaking the sound barrier
Mach 1.06 on October 14, 1947
first manned supersonic flight
|
|
gptkbp:aircraft_role
|
gptkb:aircraft
research and development
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
gptkb:Team_Rocket
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:color_scheme
|
orange and white
|
|
gptkbp:contributed_to
|
gptkb:aircraft
understanding of supersonic aerodynamics
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Glamorous_Glennis
gptkb:Team_Rocket
rocket-powered
|
|
gptkbp:design_date
|
1946
|
|
gptkbp:design_feature
|
gptkb:Team_Rocket
|
|
gptkbp:design_influence
|
gptkb:World_War_II_aircraft
modern fighter jets
future military aircraft
|
|
gptkbp:elevation
|
43,000 feet
12,000 meters
25,000 meters
|
|
gptkbp:engine_type
|
gptkb:XLR11_rocket_engine
gptkb:Team_Rocket
|
|
gptkbp:featured_in
|
various documentaries
|
|
gptkbp:first_flight
|
gptkb:66
gptkb:Chuck_Yeager
gptkb:Muroc_Army_Air_Field
1946
aerodynamic testing
engine performance testing
stability testing
October 14, 1947
control systems testing
Chalmers Goodlin
|
|
gptkbp:first_powered_flight_date
|
December 19, 1946
|
|
gptkbp:first_supersonic_flight
|
October 14, 1947
|
|
gptkbp:first_supersonic_flight_date
|
October 14, 1947
|
|
gptkbp:first_supersonic_flight_pilot
|
gptkb:Chuck_Yeager
|
|
gptkbp:fuselage_material
|
aluminum
|
|
gptkbp:height
|
2.5 m
2.5 meters
|
|
gptkbp:historical_context
|
Cold War aviation advancements
|
|
gptkbp:historical_event
|
aviation milestones
|
|
gptkbp:historical_role
|
pioneered supersonic flight
|
|
gptkbp:historical_significance
|
milestone in aviation history
first to achieve supersonic flight.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell X-1
|
|
gptkbp:impact
|
hypersonic flight
|
|
gptkbp:influenced
|
gptkb:X-15_program
gptkb:NASA's_X-15_program
NASA's space programs
design of future military aircraft
design of future supersonic aircraft
|
|
gptkbp:influenced_by
|
German rocket technology
|
|
gptkbp:inspiration
|
future supersonic aircraft
|
|
gptkbp:inspired
|
future space vehicles
commercial supersonic transport development
|
|
gptkbp:involved_in
|
gptkb:Project_Highspeed
U. S. Air Force flight testing
|
|
gptkbp:involved_in_testing
|
high-speed flight characteristics
|
|
gptkbp:is_tested_for
|
X-plane program
new flight technologies
NACA and USAF
NACA and USAF collaboration
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
paved the way for supersonic flight technology
inspired the X-series aircraft
|
|
gptkbp:length
|
8.4 meters
8.4 m
|
|
gptkbp:location
|
gptkb:Smithsonian_National_Air_and_Space_Museum
|
|
gptkbp:manufacturer
|
gptkb:Bell_Aircraft_Corporation
|
|
gptkbp:max_speed
|
Mach 1.06
|
|
gptkbp:nationality
|
gptkb:United_States
|
|
gptkbp:nickname
|
gptkb:Glamorous_Glennis
|
|
gptkbp:notable_achievement
|
first aircraft to break the sound barrier
first supersonic flight by a human-piloted aircraft
|
|
gptkbp:notable_feature
|
rocket engine propulsion
|
|
gptkbp:notable_pilots
|
gptkb:Charles_E._Yeager
gptkb:Scott_Crossfield
gptkb:Chuck_Yeager
|
|
gptkbp:number_built
|
gptkb:3
|
|
gptkbp:operated_by
|
gptkb:NACA
|
|
gptkbp:operational_period
|
1947-1958
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operational_use
|
research and testing
test flights
|
|
gptkbp:part_of
|
X-plane program
X-Plane program
|
|
gptkbp:power_source
|
4 x XLR11-BA-1 engines
|
|
gptkbp:range
|
1,600 km
|
|
gptkbp:retired
|
gptkb:1958
gptkb:NASA
|
|
gptkbp:retirement
|
gptkb:1958
completion of research objectives
|
|
gptkbp:retirement_year
|
gptkb:1956
|
|
gptkbp:role
|
gptkb:aircraft
research and development
|
|
gptkbp:service
|
gptkb:1958
1947-1958
1947-1956
|
|
gptkbp:service_ceiling
|
12,000 m
12,000 meters
|
|
gptkbp:significance
|
first aircraft to break the sound barrier
pioneering supersonic flight
pioneering supersonic flight technology
|
|
gptkbp:speed
|
1,126 km/h
|
|
gptkbp:successor
|
gptkb:X-15
gptkb:Bell_X-1_A
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:test_program_duration
|
1947-1956
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:used_for
|
aerodynamic research
|
|
gptkbp:used_in
|
aeronautical engineering studies
|
|
gptkbp:weight
|
3,175 kg
|
|
gptkbp:wing_area
|
15.5 m²
|
|
gptkbp:wing_configuration
|
high aspect ratio
straight wings
200 kg/m²
|
|
gptkbp:wingspan
|
8.4 meters
8.0 meters
8.0 m
|
|
gptkbp:bfsParent
|
gptkb:National_Air_and_Space_Museum
gptkb:Smithsonian_National_Air_and_Space_Museum
|
|
gptkbp:bfsLayer
|
3
|