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gptkbp:instanceOf
|
anti-ship missile
|
|
gptkbp:countermeasures
|
limited effectiveness against electronic countermeasures
|
|
gptkbp:deployedTo
|
naval forces
|
|
gptkbp:design
|
gptkb:Soviet_Union
anti-ship warfare
high speed and maneuverability
|
|
gptkbp:developedBy
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:developer
|
gptkb:Russia
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engineType
|
turbojet engine
|
|
gptkbp:exportedTo
|
gptkb:China
|
|
gptkbp:firstDeployment
|
1980s
|
|
gptkbp:firstFlight
|
1977
|
|
gptkbp:guidedTours
|
inertial navigation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SS-N-22 Sunburn
|
|
gptkbp:introduced
|
1980s
|
|
gptkbp:launchSite
|
surface ships
vertical launch system
cruisers and destroyers
|
|
gptkbp:length
|
8.9 m
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
|
gptkbp:militaryRank
|
gptkb:Russian_Navy
|
|
gptkbp:missileSystem
|
subsonic missile
|
|
gptkbp:notableFeature
|
engagements in naval conflicts
|
|
gptkbp:notableUsers
|
gptkb:India
|
|
gptkbp:operationalRange
|
200 km
|
|
gptkbp:operationalStatus
|
in service
naval engagements
|
|
gptkbp:productionCompany
|
operational
1970s to 1980s
|
|
gptkbp:provides
|
active radar homing
inertial guidance with terminal active radar homing
|
|
gptkbp:range
|
up to 300 km
|
|
gptkbp:relatedPatent
|
Kh-22
|
|
gptkbp:security
|
low radar cross-section
|
|
gptkbp:serviceHistory
|
used_by_Russian_Navy
|
|
gptkbp:speed
|
Mach_2.5
|
|
gptkbp:successor
|
gptkb:P-800_Oniks
BrahMos
|
|
gptkbp:supportRole
|
gptkb:Gulf_War
up to 200 km
|
|
gptkbp:targets
|
active radar seeker
surface vessels
|
|
gptkbp:team
|
Moscow_Institute_of_Thermal_Technology_team
|
|
gptkbp:technology
|
gptkb:BrahMos_missile_system
missile technology
|
|
gptkbp:type
|
high-explosive or nuclear
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingspan
|
3.0 m
|