|
gptkbp:instance_of
|
gptkb:military_aircraft
|
|
gptkbp:contract
|
gptkb:1961
|
|
gptkbp:control_surfaces
|
canards
|
|
gptkbp:crew_capacity
|
two pilots
|
|
gptkbp:design
|
gptkb:Boeing
conceptual phase
|
|
gptkbp:design_feature
|
gptkb:spacecraft
|
|
gptkbp:developed_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:duration
|
1957 to 1963
|
|
gptkbp:elevation
|
up to 100 km
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:1963
suborbital and orbital
planned but not conducted
|
|
gptkbp:fuselage_material
|
aluminum alloy
|
|
gptkbp:has_programs
|
estimated at $1 billion
|
|
gptkbp:historical_significance
|
first military spaceplane concept
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-20 Dyna-Soar program
|
|
gptkbp:influenced_by
|
gptkb:Cold_War
|
|
gptkbp:inspiration
|
gptkb:X-15_program
|
|
gptkbp:involved_technology
|
spacecraft reentry
|
|
gptkbp:is_influenced_by
|
jet propulsion
|
|
gptkbp:launch_date
|
gptkb:1963
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II
|
|
gptkbp:mission_duration
|
up to 24 hours
|
|
gptkbp:mission_type
|
gptkb:military_aircraft
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
airborne launch
|
|
gptkbp:parent_agency
|
gptkb:NASA
|
|
gptkbp:passenger_traffic
|
Mach 3
|
|
gptkbp:payload_capacity
|
3,000 pounds
|
|
gptkbp:program_goal
|
demonstrate space access
|
|
gptkbp:project
|
gptkb:Robert_E._Mc_Kee
gptkb:X-15
|
|
gptkbp:projected_cost_per_flight
|
$10 million
|
|
gptkbp:projected_crew_experience
|
extensive flight training
|
|
gptkbp:projected_crew_training
|
extensive
|
|
gptkbp:projected_flight_altitude
|
100 km
|
|
gptkbp:projected_flight_crew
|
two pilots
|
|
gptkbp:projected_impact_on_future_programs
|
influenced Space Shuttle design
|
|
gptkbp:projected_launch_frequency
|
once per month
|
|
gptkbp:projected_mission_profile
|
suborbital and orbital missions
|
|
gptkbp:projected_operational_use
|
military and intelligence purposes
|
|
gptkbp:projected_orbit
|
low Earth orbit
|
|
gptkbp:projected_payload
|
up to 3,000 pounds
|
|
gptkbp:projected_recovery_method
|
aircraft landing
|
|
gptkbp:projected_speed_range
|
Mach 3 to Mach 5
|
|
gptkbp:projected_technological_advancements
|
hypersonic technology
|
|
gptkbp:purpose
|
reconnaissance and strike missions
|
|
gptkbp:range
|
1,000 miles
|
|
gptkbp:status
|
canceled
|
|
gptkbp:successor
|
gptkb:Space_Shuttle
|
|
gptkbp:technology
|
hypersonic flight
|
|
gptkbp:termination_year
|
gptkb:1963
|
|
gptkbp:weight
|
approximately 15,000 pounds
|
|
gptkbp:wing_configuration
|
approximately 30 feet
|
|
gptkbp:bfsParent
|
gptkb:X-15_rocket_plane_program
|
|
gptkbp:bfsLayer
|
6
|