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gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:ceiling
|
15,000 m
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:deployment
|
air-launched
|
|
gptkbp:design_features
|
swept wings
|
|
gptkbp:designated_as
|
gptkb:USAF
|
|
gptkbp:developed_by
|
gptkb:North_American_Aviation
|
|
gptkbp:development
|
1954-1959
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:exported_to
|
gptkb:none
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_type
|
gptkb:RP-1/_LOX
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
1,000 m
inertial guidance
|
|
gptkbp:has_ability
|
gptkb:1960
|
|
gptkbp:has_programs
|
SM-68
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SM-65
|
|
gptkbp:is_targeted_at
|
fixed targets
|
|
gptkbp:launch_platform
|
gptkb:aircraft
|
|
gptkbp:launch_vehicle
|
gptkb:aircraft
|
|
gptkbp:launch_window
|
airborne launch
|
|
gptkbp:length
|
8.4 m
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:max_takeoff_weight
|
3,000 kg
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:primary_user
|
gptkb:United_States_Air_Force
|
|
gptkbp:propulsion
|
liquid propulsion
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement
|
technological obsolescence
|
|
gptkbp:retirement_year
|
gptkb:1980
|
|
gptkbp:role
|
strategic standoff weapon
|
|
gptkbp:service_entry
|
gptkb:1959
|
|
gptkbp:speed
|
Mach 3
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:AGM-86_ALCM
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:warhead_type
|
nuclear
up to 1.2 megatons
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
8.2 m
|
|
gptkbp:bfsParent
|
gptkb:Atlas_F
|
|
gptkbp:bfsLayer
|
6
|