|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Hercules_X-20
gptkb:X-15_Rocket_Plane
|
|
gptkbp:aircraft_operated
|
gptkb:auto_race
gptkb:Robert_White
up to 100 km
|
|
gptkbp:allows
|
limited funding
|
|
gptkbp:budget
|
$1 billion
|
|
gptkbp:cancellation_reason
|
gptkb:1963
budget cuts
|
|
gptkbp:challenges
|
thermal protection
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
2
|
|
gptkbp:date
|
gptkb:1957
|
|
gptkbp:design
|
gptkb:Hugh_Dryden
gptkb:aircraft
gptkb:spacecraft
gptkb:Robert_Mc_Donnell
completed in 1960
multiple prototypes
NASA and USAF
North American Aviation engineers
reusable space vehicle
|
|
gptkbp:developer
|
gptkb:1957
|
|
gptkbp:duration
|
6 years
1957-1963
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:features
|
delta wing
|
|
gptkbp:first_flight
|
gptkb:none
gptkb:1963
planned but not executed
1963-12-06
|
|
gptkbp:first_introduced
|
gptkb:1957
|
|
gptkbp:fuel_type
|
liquid oxygen and kerosene
|
|
gptkbp:has_programs
|
gptkb:Dyna-Soar_program
gptkb:Colonel_William_M._Mc_Culloch
|
|
gptkbp:height
|
4.6 meters
|
|
gptkbp:historical_significance
|
first military spaceplane concept
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-20 Dyna-Soar
|
|
gptkbp:influenced_by
|
gptkb:Mercury_program
gptkb:X-15_program
gptkb:Gemini_program
U. S. Air Force needs
|
|
gptkbp:inspiration
|
gptkb:aircraft
gptkb:spacecraft
|
|
gptkbp:invention
|
2
|
|
gptkbp:is_capable_of
|
suborbital and orbital flight
|
|
gptkbp:is_influenced_by
|
aerodynamics research
jet propulsion
|
|
gptkbp:is_involved_in
|
gptkb:Monarch
|
|
gptkbp:launch_date
|
gptkb:1965
|
|
gptkbp:launch_site
|
gptkb:cape
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_II
|
|
gptkbp:legacy
|
provided data for future missions
influenced future space missions
influenced future space programs
contributed to spaceplane design
|
|
gptkbp:length
|
15.2 meters
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Aircraft_Corporation
gptkb:North_American_Aviation
|
|
gptkbp:max_speed
|
Mach 3.5
Mach 6.5
|
|
gptkbp:max_takeoff_weight
|
runway landing
|
|
gptkbp:mission
|
orbital reconnaissance
|
|
gptkbp:notable_feature
|
modular design
advanced avionics
reusable components
thermal protection system
multi-role capability
high altitude operation
crew escape system
horizontal landing
vertical takeoff
experimental technology
suborbital flight capability
winged design
|
|
gptkbp:operated_by
|
gptkb:aircraft
|
|
gptkbp:operational_area
|
1960s
reconnaissance and strike
1963-1963
|
|
gptkbp:operational_status
|
canceled
|
|
gptkbp:performance
|
up to 24 hours
|
|
gptkbp:project
|
gptkb:Manned_Orbiting_Laboratory
|
|
gptkbp:purpose
|
gptkb:aircraft
|
|
gptkbp:related_concept
|
gptkb:1956
|
|
gptkbp:related_to
|
gptkb:US_Air_Force
gptkb:X-15
gptkb:NASA
|
|
gptkbp:research_and_development
|
military space program
|
|
gptkbp:retired
|
gptkb:1963
|
|
gptkbp:status
|
canceled
never flew
|
|
gptkbp:successor
|
gptkb:spacecraft
gptkb:none
|
|
gptkbp:targets
|
1,000 kg
|
|
gptkbp:technology
|
aerodynamic design
hypersonic flight
reentry vehicle
|
|
gptkbp:weight
|
6,000 kg
|
|
gptkbp:wingspan
|
8.5 meters
8.4 meters
|