|
gptkbp:instance_of
|
gptkb:aircraft
gptkb:concept
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Hercules_X-20
|
|
gptkbp:aircraft_operated
|
fly-by-wire system
Mach 5+
|
|
gptkbp:artistic_influence
|
gptkb:NASA's_Space_Shuttle_program
|
|
gptkbp:avionics
|
advanced avionics
|
|
gptkbp:benefits
|
cancellation
not fully realized
evaluated by military experts
shaped future aerospace research
shaped aerospace engineering
|
|
gptkbp:cancellation_reason
|
budget constraints
budget cuts
|
|
gptkbp:challenges
|
thermal protection
thermal protection system
funding and political support
|
|
gptkbp:collaborations
|
collaboration with universities
military and civilian agencies
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
2
1-2 crew members
|
|
gptkbp:debut_year
|
gptkb:1956
|
|
gptkbp:design
|
gptkb:aircraft
conceptual design
high-speed flight
1957-1963
Boeing engineers
multiple design iterations
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:developed_by
|
gptkb:aircraft
|
|
gptkbp:developer
|
1956-1963
|
|
gptkbp:elevation
|
up to 100 km
30,000 meters
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:features
|
gptkb:spacecraft
winged spaceplane
|
|
gptkbp:first_flight
|
gptkb:1963
none conducted
limited flight testing
suborbital and orbital missions
unmanned test flights
|
|
gptkbp:has_documentation
|
limited availability
extensive documentation
archived
|
|
gptkbp:has_programs
|
gptkb:aircraft
gptkb:Manned_Orbiting_Laboratory
|
|
gptkbp:height
|
4.6 meters
|
|
gptkbp:historical_context
|
Cold War era
post-Sputnik era
|
|
gptkbp:historical_significance
|
early spaceplane concept
first military spaceplane concept
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dyna-Soar
|
|
gptkbp:influenced_by
|
gptkb:X-15_program
gptkb:X-15
|
|
gptkbp:inspiration
|
gptkb:Author
gptkb:Monarch
|
|
gptkbp:invention
|
gptkb:X-20
not built
|
|
gptkbp:launch_date
|
gptkb:1963
|
|
gptkbp:launch_site
|
gptkb:cape
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II
|
|
gptkbp:launched
|
air launch
|
|
gptkbp:legacy
|
influenced future space programs
|
|
gptkbp:length
|
15.2 meters
|
|
gptkbp:manufacturer
|
gptkb:aircraft
|
|
gptkbp:max_speed
|
Mach 3.5
|
|
gptkbp:max_takeoff_weight
|
runway landing
|
|
gptkbp:mission
|
suborbital flight
|
|
gptkbp:objective
|
high-speed flight
military and civilian applications
|
|
gptkbp:operational_area
|
gptkb:aircraft
gptkb:government_agency
gptkb:none
reconnaissance missions
space-based reconnaissance
|
|
gptkbp:produced_by
|
canceled
cancelled
|
|
gptkbp:project
|
gptkb:Robert_E._Mc_Kee
gptkb:Robert_A._Mc_Donald
6 years
1955-1963
1957-1963
manned space operations
advanced aerospace capabilities
develop advanced aerospace technologies
military aerospace project
military dominance in space
|
|
gptkbp:purpose
|
gptkb:aircraft
reconnaissance
|
|
gptkbp:range
|
5000 kilometers
|
|
gptkbp:receives_funding_from
|
gptkb:aircraft
gptkb:Police_Department
gptkb:fund
gptkb:NASA
|
|
gptkbp:related_concept
|
gptkb:1955
|
|
gptkbp:related_to
|
gptkb:X-20_Dyna-Soar
hypersonic flight
|
|
gptkbp:specifies
|
gptkb:market
|
|
gptkbp:successor
|
gptkb:spacecraft
gptkb:X-37_B
|
|
gptkbp:technology
|
gptkb:spacecraft
hypersonic flight
spacecraft reentry
|
|
gptkbp:weight
|
10,000 kg
approximately 15,000 kg
|
|
gptkbp:wingspan
|
8.4 meters
|
|
gptkbp:year
|
gptkb:1957
gptkb:1963
|