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gptkbp:instance_of
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gptkb:missile
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gptkbp:associated_with
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nuclear deterrence
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gptkbp:challenges
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technical difficulties
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gptkbp:control_surfaces
|
tail fins
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gptkbp:deployment
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gptkb:aircraft
gptkb:1959
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gptkbp:design
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Douglas engineers
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gptkbp:design_features
|
airframe design for high speed
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gptkbp:designed_for
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nuclear delivery
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gptkbp:developed_by
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gptkb:United_States
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gptkbp:development
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gptkb:1955
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gptkbp:diameter
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1.0 m
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gptkbp:engine_type
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gptkb:turbofan_engine
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gptkbp:first_flight
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gptkb:1956
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gptkbp:funding
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gptkb:US_Department_of_Defense
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gptkbp:guidance_system
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gptkb:navigation_system
inertial guidance
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gptkbp:has_programs
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gptkb:1962
Skybolt program
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gptkbp:historical_significance
|
Cold War era missile development
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https://www.w3.org/2000/01/rdf-schema#label
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Skybolt missile
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gptkbp:influenced_by
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Cold War tensions
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gptkbp:is_targeted_at
|
pre-programmed targets
|
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gptkbp:is_tested_for
|
multiple successful tests
1956-1959
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gptkbp:launch_platform
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gptkb:B-52_Stratofortress
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|
gptkbp:launch_window
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air-launched
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gptkbp:legacy
|
influenced future missile designs
|
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gptkbp:length
|
8.5 m
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gptkbp:manufacturer
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gptkb:Douglas_Aircraft_Company
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|
gptkbp:max_takeoff_weight
|
2,500 kg
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:operational_status
|
canceled
|
|
gptkbp:operational_use
|
not used in combat
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:political_impact
|
influenced US-UK relations
|
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gptkbp:project_cancellation
|
due to budget cuts
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gptkbp:range
|
1,500 km
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gptkbp:retired
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gptkb:1962
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gptkbp:retirement
|
strategic shift
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gptkbp:service_frequency
|
1959-1962
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gptkbp:speed
|
Mach 3.5
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gptkbp:status
|
canceled
canceled program
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gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:strategic_importance
|
deterrent against Soviet Union
|
|
gptkbp:successor
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gptkb:AGM-86_ALCM
|
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gptkbp:type
|
gptkb:missile
|
|
gptkbp:warhead_type
|
thermonuclear
1.2 megatons
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gptkbp:weight
|
2,500 kg
|
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gptkbp:wingspan
|
6.1 m
|