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gptkbp:instance_of
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gptkb:missile
|
|
gptkbp:associated_with
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gptkb:Royal_Air_Force
|
|
gptkbp:cancellation_reason
|
budget constraints
|
|
gptkbp:debut
|
gptkb:1964
gptkb:1965
|
|
gptkbp:design
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gptkb:Avro
1955-1960
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|
gptkbp:developed_by
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gptkb:British_government
|
|
gptkbp:development
|
1947
|
|
gptkbp:development_cost
|
£100 million
|
|
gptkbp:diameter
|
2.4 meters
|
|
gptkbp:engine_type
|
liquid-fueled rocket engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:historical_significance
|
early British missile development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Blue Streak program
|
|
gptkbp:influenced_by
|
gptkb:Cold_War
|
|
gptkbp:involved_countries
|
gptkb:Australia
gptkb:United_Kingdom
|
|
gptkbp:involved_technology
|
to Australia
|
|
gptkbp:is_tested_for
|
gptkb:3
|
|
gptkbp:launch_mass
|
30,000 kg
|
|
gptkbp:launch_platform
|
gptkb:ground
ground launch
|
|
gptkbp:launch_site
|
gptkb:Woomera_Test_Range
|
|
gptkbp:launch_vehicle
|
gptkb:Blue_Streak_rocket
|
|
gptkbp:launched
|
gptkb:5
|
|
gptkbp:legacy
|
influenced future missile programs
|
|
gptkbp:length
|
25.6 meters
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_period
|
1955-1960
|
|
gptkbp:operational_range
|
4,000 km
|
|
gptkbp:payload_capacity
|
1,000 kg
|
|
gptkbp:project
|
gptkb:Sir_Frederick_Page
gptkb:military_campaigns
gptkb:Skybolt_missile
gptkb:Blue_Streak
|
|
gptkbp:propulsion
|
kerosene and liquid oxygen
1,000 k N
|
|
gptkbp:purpose
|
gptkb:missile
|
|
gptkbp:range
|
4,000 km
|
|
gptkbp:related_to
|
British nuclear deterrent
|
|
gptkbp:result
|
gptkb:1960
cancellation
|
|
gptkbp:status
|
canceled
|
|
gptkbp:successor
|
gptkb:Polaris_submarine-launched_ballistic_missile
|
|
gptkbp:weight
|
30,000 kg
|