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gptkbp:instance_of
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gptkb:missile
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gptkbp:armament
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gptkb:Kh-22
|
|
gptkbp:challenges
|
technological limitations
|
|
gptkbp:combat_history
|
limited use in Cold War
|
|
gptkbp:combat_role
|
strategic strike weapon
|
|
gptkbp:control_surfaces
|
canards
|
|
gptkbp:counterpart
|
U. S. Tomahawk missile
|
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gptkbp:decommissioned
|
gptkb:Russian_Federation
|
|
gptkbp:deployment
|
gptkb:Soviet_Armed_Forces
mobile launchers
|
|
gptkbp:design
|
Vympel Design Bureau team
A. A. Raspletin
|
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gptkbp:design_features
|
modular design
high speed and range
|
|
gptkbp:design_purpose
|
anti-ship and land attack
strategic strike
|
|
gptkbp:designed_by
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
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gptkbp:developed_by
|
gptkb:Soviet_Union
|
|
gptkbp:development
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gptkb:1965
1970s
1965-1970
|
|
gptkbp:development_cost
|
classified
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
liquid-fueled engine
|
|
gptkbp:exported_to
|
no known exports
|
|
gptkbp:fighting_style
|
gptkb:none
|
|
gptkbp:final_service_year
|
gptkb:1995
|
|
gptkbp:first_flight
|
gptkb:1970
gptkb:1975
successful
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:guidance_system
|
gptkb:100_meters
10 meters
inertial guidance
inertial guidance system
terminal homing
|
|
gptkbp:has_ability
|
gptkb:1972
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-2700 missile
|
|
gptkbp:influence_on
|
subsequent missile designs
|
|
gptkbp:influenced_by
|
Kh-22 missile design
|
|
gptkbp:is_targeted_at
|
gptkb:radar_system
radar guidance
|
|
gptkbp:is_tested_for
|
gptkb:Kapustin_Yar
1968-1970
multiple successful tests
completed in 1975
|
|
gptkbp:launch_platform
|
gptkb:ground
ground-based launcher
mobile launcher
manual and automated
|
|
gptkbp:launch_vehicle
|
ground-based launcher
|
|
gptkbp:launch_window
|
vertical launch
|
|
gptkbp:launched
|
30 degrees
vertical launch
|
|
gptkbp:legacy
|
influenced missile technology
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:location
|
gptkb:Eastern_Europe
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
gptkb:Vympel_Design_Bureau
|
|
gptkbp:max_takeoff_weight
|
3,000 kg
3,500 kg
|
|
gptkbp:military_branch
|
gptkb:Soviet_Air_Force
|
|
gptkbp:modifications
|
R-2700 M
|
|
gptkbp:operational_range
|
250 km
1,500 km
|
|
gptkbp:operational_status
|
obsolete
|
|
gptkbp:operational_theater
|
gptkb:Europe
|
|
gptkbp:operational_use
|
limited
strategic deterrence
|
|
gptkbp:propulsion
|
gptkb:turbofan_engine
|
|
gptkbp:range
|
250 km
2,500 km
|
|
gptkbp:research_institutes
|
gptkb:Moscow_Institute_of_Physics_and_Technology
|
|
gptkbp:retirement
|
technological obsolescence
|
|
gptkbp:retirement_year
|
gptkb:1990
1990s
|
|
gptkbp:role
|
tactical strike
|
|
gptkbp:service_entry
|
gptkb:1980s
|
|
gptkbp:service_history
|
gptkb:Cold_War
|
|
gptkbp:speed
|
Mach 3
Mach 0.9
|
|
gptkbp:status
|
retired
|
|
gptkbp:stealth_features
|
yes
limited
low radar cross-section
|
|
gptkbp:strategic_importance
|
high during Cold War
|
|
gptkbp:successor
|
gptkb:P-800_Oniks
R-300 missile
R-2700 M missile
|
|
gptkbp:system
|
gptkb:R-15_missile
|
|
gptkbp:targets
|
land and naval targets
|
|
gptkbp:treaty
|
gptkb:START_I
|
|
gptkbp:type
|
gptkb:missile
|
|
gptkbp:used_by
|
gptkb:Soviet_Union
|
|
gptkbp:used_in
|
1990s
|
|
gptkbp:warhead_type
|
1,000 kg
nuclear
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
8.0 meters
|