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gptkbp:instanceOf
|
missile
|
|
gptkbp:deployedTo
|
air-launched
|
|
gptkbp:design
|
land attack
anti-ship
|
|
gptkbp:designedBy
|
gptkb:Raduga_Design_Bureau
|
|
gptkbp:engineType
|
turbojet engine
|
|
gptkbp:exportedTo
|
gptkb:Egypt
gptkb:India
gptkb:Syria
gptkb:Iraq
gptkb:Libya
|
|
gptkbp:firstFlight
|
1951
|
|
gptkbp:fuelType
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Raduga missile
|
|
gptkbp:launchSite
|
gptkb:Tu-16
gptkb:Tu-4
Tu-95
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Raduga_Design_Bureau
|
|
gptkbp:notableUsers
|
gptkb:Algerian_Air_Force
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force
gptkb:Syrian_Air_Force
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force
gptkb:Angolan_Air_Force
gptkb:Iraqi_Air_Force
gptkb:Libyan_Air_Force
gptkb:Vietnam_People's_Air_Force
|
|
gptkbp:operationalRange
|
600 km
|
|
gptkbp:productionCompany
|
1947-1953
|
|
gptkbp:provides
|
active radar homing
inertial guidance
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:security
|
limited radar cross-section
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:services
|
1953
|
|
gptkbp:speed
|
0.9 Mach
|
|
gptkbp:successor
|
Kh-22
Kh-15
|
|
gptkbp:supportRole
|
gptkb:Vietnam_War
gptkb:Arab-Israeli_conflict
|
|
gptkbp:targets
|
ground targets
|
|
gptkbp:type
|
cruise missile
nuclear
|
|
gptkbp:usedBy
|
gptkb:Soviet_Union
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
8.0 m
|