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gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:ceiling
|
20,000 m
|
|
gptkbp:combat_radius
|
80 km
|
|
gptkbp:deployment
|
gptkb:naval_warfare
aircraft carriers
land bases
|
|
gptkbp:diameter
|
0.23 m
|
|
gptkbp:fighting_style
|
air superiority missions
|
|
gptkbp:guidance_system
|
semi-active radar homing
inertial guidance system
|
|
gptkbp:historical_significance
|
Cold War era weapon
Soviet military innovation
modern air combat technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-27 ER missile
|
|
gptkbp:is_targeted_at
|
gptkb:aircraft
gptkb:drones
missiles
|
|
gptkbp:launch_platform
|
gptkb:Su-30
gptkb:Su-27
gptkb:Mi_G-29
|
|
gptkbp:launched
|
vertical launch
angled launch
|
|
gptkbp:length
|
4.0 m
|
|
gptkbp:manufacturer
|
gptkb:Vympel
|
|
gptkbp:modifications
|
enhanced guidance systems
upgraded electronics
improved propulsion
|
|
gptkbp:operational_status
|
in service
combat ready
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:propulsion
|
solid rocket motor
|
|
gptkbp:provides_guidance_on
|
active radar homing
|
|
gptkbp:range
|
130 km
|
|
gptkbp:related_to
|
R-27 missile family
|
|
gptkbp:service_entry
|
gptkb:1980s
|
|
gptkbp:speed
|
Mach 4.0
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:successor
|
gptkb:R-77_missile
|
|
gptkbp:training
|
pilot training
missile systems training
|
|
gptkbp:used_by
|
gptkb:Russian_Air_Force
|
|
gptkbp:user_countries
|
gptkb:China
gptkb:India
gptkb:Kazakhstan
gptkb:Ukraine
gptkb:Belarus
|
|
gptkbp:variant
|
gptkb:R-27_R
gptkb:R-27_T
|
|
gptkbp:warhead_type
|
high-explosive
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:wingspan
|
2.0 m
|
|
gptkbp:bfsParent
|
gptkb:Vympel_Design_Bureau
|
|
gptkbp:bfsLayer
|
6
|