|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
manual and automated
|
|
gptkbp:avionics
|
advanced for its time
|
|
gptkbp:budget
|
$1 billion
|
|
gptkbp:cancellation_reason
|
gptkb:1963
|
|
gptkbp:challenges
|
thermal protection
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:cooling_system
|
ablative
|
|
gptkbp:crew_capacity
|
2
|
|
gptkbp:design
|
gptkb:Mc_Donnell_Aircraft_Corporation
completed
|
|
gptkbp:design_features
|
delta wing
|
|
gptkbp:design_purpose
|
gptkb:spacecraft
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
1957-1963
|
|
gptkbp:duration
|
6 years
|
|
gptkbp:elevation
|
up to 100 km
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:1963
suborbital
none conducted
|
|
gptkbp:fuselage_material
|
aluminum alloy
|
|
gptkbp:has_programs
|
Robert E. Gilruth
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dyna-Soar X-20
|
|
gptkbp:inception
|
gptkb:1957
|
|
gptkbp:influenced_by
|
gptkb:X-15_program
|
|
gptkbp:inspiration
|
gptkb:Space_Shuttle
|
|
gptkbp:is_influenced_by
|
spaceplane design
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II
|
|
gptkbp:legacy
|
influenced future space missions
|
|
gptkbp:length
|
15.2 meters
|
|
gptkbp:max_speed
|
Mach 3.5
|
|
gptkbp:mission_duration
|
up to 24 hours
|
|
gptkbp:mission_type
|
reconnaissance and research
|
|
gptkbp:operational_use
|
low Earth orbit
not realized
|
|
gptkbp:origin
|
gptkb:United_States_Air_Force
|
|
gptkbp:passenger_traffic
|
up to Mach 5
|
|
gptkbp:project
|
gptkb:Manned_Orbiting_Laboratory
|
|
gptkbp:projected_altitude
|
up to 150 km
|
|
gptkbp:projected_crew_experience
|
highly trained pilots
|
|
gptkbp:projected_crew_training
|
extensive
|
|
gptkbp:projected_flight_time
|
up to 2 hours
|
|
gptkbp:projected_landing_method
|
runway landing
|
|
gptkbp:projected_launch_frequency
|
1 per year
|
|
gptkbp:projected_payload
|
1,000 kg
|
|
gptkbp:projected_recovery_method
|
aircraft recovery
|
|
gptkbp:propulsion
|
100,000 lbf
|
|
gptkbp:purpose
|
gptkb:military_aircraft
|
|
gptkbp:range
|
1,000 miles
|
|
gptkbp:related_vehicle
|
yes
|
|
gptkbp:status
|
canceled
|
|
gptkbp:weight
|
6,000 kg
|
|
gptkbp:wingspan
|
8.5 meters
|
|
gptkbp:bfsParent
|
gptkb:Dyna-Soar_program
|
|
gptkbp:bfsLayer
|
7
|