|
gptkbp:instanceOf
|
cruise missile
|
|
gptkbp:associatedAct
|
gptkb:Soviet_Union
|
|
gptkbp:deployedTo
|
gptkb:Cold_War
|
|
gptkbp:design
|
gptkb:Soviet_Union
high maneuverability
anti-ship warfare
|
|
gptkbp:designedBy
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:developer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:electronic_warfare
|
limited use in naval engagements
|
|
gptkbp:engineType
|
turbojet
|
|
gptkbp:exportedTo
|
no known exports
|
|
gptkbp:firstDeployment
|
1975
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:historicalSignificance
|
Cold_War_naval_strategy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SS-N-16
|
|
gptkbp:launchSite
|
submarine
vertical launch system
|
|
gptkbp:launchVehicle
|
submarine-launched
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
|
gptkbp:militaryRank
|
naval forces
|
|
gptkbp:notableFeature
|
high speed and range
|
|
gptkbp:operationalRange
|
600 km
|
|
gptkbp:operationalStatus
|
retired
naval warfare
limited_to_Soviet_Navy
|
|
gptkbp:previouslyKnownAs
|
1990s
|
|
gptkbp:productionCompany
|
1960s to 1970s
|
|
gptkbp:propulsion
|
turbojet engine
|
|
gptkbp:provides
|
inertial guidance with terminal active radar homing
|
|
gptkbp:range
|
600 km
|
|
gptkbp:relatedPatent
|
gptkb:SS-N-15
|
|
gptkbp:resources
|
inertial and terminal guidance
|
|
gptkbp:retirementYear
|
1990s
|
|
gptkbp:secondaryRole
|
anti-ship missile
land attack
|
|
gptkbp:security
|
limited radar cross-section
|
|
gptkbp:services
|
1975
|
|
gptkbp:speed
|
Mach_0.9
|
|
gptkbp:successor
|
gptkb:SS-N-22_Sunburn
gptkb:SS-N-22
|
|
gptkbp:targets
|
active radar homing
surface ships
|
|
gptkbp:type
|
600 kg
anti-ship missile
nuclear
|
|
gptkbp:usedBy
|
gptkb:Soviet_Navy
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
6.5 meters
|