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gptkbp:instance_of
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gptkb:missile
|
|
gptkbp:armament
|
gptkb:MIM-23_Hawk
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|
gptkbp:combat_radius
|
15 km
|
|
gptkbp:combat_role
|
air defense
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:deployment
|
gptkb:1980s
ground-based air defense
|
|
gptkbp:design_date
|
1960s
|
|
gptkbp:designed_by
|
gptkb:Raytheon
|
|
gptkbp:development
|
1960s to 1980s
Hawk missile system
|
|
gptkbp:diameter
|
0.15 m
|
|
gptkbp:elevation
|
8 km
|
|
gptkbp:engine_type
|
solid rocket motor
|
|
gptkbp:fighting_style
|
gptkb:Gulf_War
|
|
gptkbp:first_flight
|
1970s
|
|
gptkbp:guidance_system
|
semi-active radar homing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
MIM-23 C
|
|
gptkbp:introduced_in
|
gptkb:1980s
|
|
gptkbp:is_integrated_with
|
integrated with radar systems
|
|
gptkbp:is_targeted_at
|
radar guidance
|
|
gptkbp:launch_platform
|
gptkb:M113_armored_personnel_carrier
mobile launcher
|
|
gptkbp:launched
|
vertical launch
|
|
gptkbp:length
|
3.66 m
|
|
gptkbp:manufacturer
|
gptkb:Raytheon_Company
|
|
gptkbp:max_takeoff_weight
|
200 kg
|
|
gptkbp:military_branch
|
gptkb:Army
|
|
gptkbp:operational_range
|
10 km
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:propulsion
|
solid-fuel rocket motor
|
|
gptkbp:provides_guidance_on
|
active radar homing
|
|
gptkbp:range
|
15 km
|
|
gptkbp:related_to
|
gptkb:MIM-23_Hawk
|
|
gptkbp:replaced_by
|
gptkb:MIM-104_Patriot
|
|
gptkbp:retirement_year
|
still in service
|
|
gptkbp:role
|
air defense
|
|
gptkbp:service_history
|
used in various conflicts
|
|
gptkbp:speed
|
Mach 2.5
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:MIM-104_Patriot
|
|
gptkbp:system
|
gptkb:missile
|
|
gptkbp:targets
|
gptkb:aircraft
|
|
gptkbp:type
|
gptkb:missile
|
|
gptkbp:used_by
|
gptkb:United_States_Army
|
|
gptkbp:user_countries
|
gptkb:United_States
|
|
gptkbp:warhead_type
|
high-explosive
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:wingspan
|
1.2 m
|
|
gptkbp:bfsParent
|
gptkb:MIM-23_Hawk
|
|
gptkbp:bfsLayer
|
6
|