|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:X-24
|
|
gptkbp:affiliated_with
|
gptkb:NASA_Langley_Research_Center
|
|
gptkbp:aircraft_operated
|
gptkb:Robert_White
gptkb:Joe_Walker
gptkb:first_powered_flight
gptkb:William_J._
automated systems
experimental
fly-by-wire
up to 30 minutes
high-mounted wings
suborbital vehicle
50 pounds per square foot
up to 100,000 feet
|
|
gptkbp:analysis
|
flight dynamics
|
|
gptkbp:aspect_ratio
|
2.5
|
|
gptkbp:clinical_trial
|
30 minutes
|
|
gptkbp:collaborations
|
gptkb:aircraft
gptkb:US_Air_Force
NASA and USAF
|
|
gptkbp:collection
|
aerodynamic performance
aerodynamic data
|
|
gptkbp:contribution
|
hypersonic flight research
|
|
gptkbp:controls
|
fly-by-wire
elevons
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:data_usage
|
NASA research
|
|
gptkbp:decommissioned
|
gptkb:1970
|
|
gptkbp:design
|
gptkb:NASA_Langley_Research_Center
rocket-powered
lifting body
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:first_flight
|
gptkb:12
gptkb:1966
gptkb:1970
gptkb:27
gptkb:California
gptkb:Edwards_Air_Force_Base
1970s
Phase II
extensive
over 20
suborbital
successful missions
suborbital trajectory
stable at high speeds
advancements in aerospace engineering
developmental testing
June 12, 1969
validated design concepts
incremental testing
evaluate aerodynamic performance
recorded telemetry
steep climb and glide descent
|
|
gptkbp:fuel_capacity
|
1,000 pounds
|
|
gptkbp:has_authority_over
|
high angle of attack
|
|
gptkbp:has_programs
|
HL-10
|
|
gptkbp:height
|
6.5 feet
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-24 A
|
|
gptkbp:impact
|
advanced flight control systems
|
|
gptkbp:influence
|
modern aerospace engineering
|
|
gptkbp:influenced
|
modern aircraft design
|
|
gptkbp:influenced_by
|
gptkb:X-15
|
|
gptkbp:inspiration
|
future space vehicles
|
|
gptkbp:is_involved_in
|
aeronautical research
|
|
gptkbp:is_tested_for
|
Flight Research Center
validated aerodynamic theories
|
|
gptkbp:landing_gear
|
gptkb:horse_race
|
|
gptkbp:launch_site
|
gptkb:B-52_Stratofortress
gptkb:Edwards_Air_Force_Base
|
|
gptkbp:legacy
|
influenced future aircraft designs
advanced aerospace technology
|
|
gptkbp:length
|
15.24 meters
16.8 feet
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:material
|
aluminum alloy
delta wing
|
|
gptkbp:max_speed
|
gptkb:Mach_3.0
|
|
gptkbp:mission
|
evaluate stability and control
|
|
gptkbp:operational_area
|
1969-1975
research and development
1966-1970
|
|
gptkbp:operational_range
|
100 km
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:project
|
gptkb:Dyna-Soar
|
|
gptkbp:propulsion
|
15,000 pounds
|
|
gptkbp:purpose
|
gptkb:Research_Institute
research and development
|
|
gptkbp:related_to
|
spaceplane development
|
|
gptkbp:research
|
improved flight stability
improved understanding of hypersonic flight
|
|
gptkbp:research_areas
|
hypersonic flight
|
|
gptkbp:research_focus
|
aerodynamics
|
|
gptkbp:retirement_year
|
gptkb:1975
|
|
gptkbp:role
|
suborbital flight testing
|
|
gptkbp:roll_rate
|
10 degrees per second
|
|
gptkbp:setting
|
tailless
|
|
gptkbp:significance
|
pioneering hypersonic flight
contributed to space shuttle design
|
|
gptkbp:speed
|
100 knots
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:X-24_B
|
|
gptkbp:surface
|
elevons
canards
|
|
gptkbp:tail_type
|
no vertical tail
|
|
gptkbp:used_in
|
gptkb:X-15_program
|
|
gptkbp:weight
|
3,000 pounds
3,600 kg
|
|
gptkbp:wingspan
|
22.5 feet
8.23 meters
|