|
gptkbp:instanceOf
|
experimental aircraft
|
|
gptkbp:aircraft
|
gptkb:Bell_X-1
experimental
monoplane
supersonic aircraft
research aircraft
straight wings
|
|
gptkbp:cockpit
|
gptkb:Chuck_Yeager
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
gptkb:Scott_Crossfield
1
|
|
gptkbp:decommissioned
|
1960
|
|
gptkbp:design
|
rocket-powered aircraft
|
|
gptkbp:design_feature
|
rocket propulsion system
|
|
gptkbp:engineType
|
Rocket engine
|
|
gptkbp:firstFlight
|
1956
over 100
|
|
gptkbp:fuelType
|
liquid propellant
|
|
gptkbp:height
|
2.74 m
|
|
gptkbp:historical_significance
|
pioneered supersonic flight research
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell X-1A
|
|
gptkbp:influenced
|
future supersonic aircraft designs
high-speed flight technology
|
|
gptkbp:inspiration
|
gptkb:NASA's_X-15_program
|
|
gptkbp:is_used_in
|
gptkb:United_States_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.53 m
|
|
gptkbp:manufacturer
|
gptkb:Bell_Aircraft_Corporation
|
|
gptkbp:maximum_speed
|
Mach_2.5
|
|
gptkbp:maxRange
|
30,000 m
|
|
gptkbp:notable_event
|
first aircraft to fly at Mach 2.5
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:purpose
|
research and development
|
|
gptkbp:retired
|
1960
|
|
gptkbp:role
|
supersonic flight testing
|
|
gptkbp:serviceType
|
1956-1960
|
|
gptkbp:significance
|
first aircraft to exceed Mach 2
|
|
gptkbp:successor
|
Bell X-1B
|
|
gptkbp:team
|
Bell_Aircraft_engineers
|
|
gptkbp:training
|
X-plane program
|
|
gptkbp:weight
|
3,175 kg
|
|
gptkbp:wingspan
|
10.67 m
|