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gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:aircraft_operated
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gptkb:aircraft
first aircraft to exceed Mach 2
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gptkbp:cockpit
|
single-seat
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|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
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|
gptkbp:control_system
|
fly-by-wire
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|
gptkbp:crew
|
gptkb:1
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gptkbp:decommissioned
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gptkb:1960
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|
gptkbp:design
|
gptkb:Team_Rocket
Bell Aircraft engineers
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gptkbp:elevation
|
20,000 m
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|
gptkbp:engine
|
gptkb:Pratt_&_Whitney
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gptkbp:engine_type
|
turbojet
J57
|
|
gptkbp:first_flight
|
gptkb:1956
over 50
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gptkbp:fuel_capacity
|
1,500 liters
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|
gptkbp:fuselage_material
|
aluminum
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gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bell X-1 B
|
|
gptkbp:influenced
|
gptkb:NASA's_X-series_aircraft
future supersonic aircraft designs
|
|
gptkbp:invention
|
gptkb:1
|
|
gptkbp:is_tested_for
|
high-speed flight testing
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
pioneering supersonic flight technology
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Bell_Aircraft_Corporation
|
|
gptkbp:max_speed
|
Mach 2.5
|
|
gptkbp:max_takeoff_weight
|
4,500 kg
|
|
gptkbp:notable_achievement
|
first sustained supersonic flight
|
|
gptkbp:notable_feature
|
gptkb:Team_Rocket
high thrust-to-weight ratio
advanced avionics system
streamlined fuselage
high-speed aerodynamic design
|
|
gptkbp:notable_pilots
|
gptkb:Charles_E._Yeager
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operational_use
|
research and development
|
|
gptkbp:purpose
|
gptkb:research
|
|
gptkbp:release_date
|
gptkb:1955
|
|
gptkbp:retired
|
gptkb:1960
|
|
gptkbp:roll_rate
|
30 degrees per second
|
|
gptkbp:service
|
1956-1960
|
|
gptkbp:stall_speed
|
150 knots
|
|
gptkbp:successor
|
gptkb:Bell_X-1
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:used_for
|
aerodynamic research
|
|
gptkbp:weight
|
3,600 kg
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
9.1 m
|
|
gptkbp:bfsParent
|
gptkb:Bell_X-1_A
|
|
gptkbp:bfsLayer
|
5
|