Kh-65M

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instanceOf gptkb:spacecraft
gptkbp:deployedTo air-launched
gptkbp:design high maneuverability
to engage high-value targets
gptkbp:designedBy gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:developer gptkb:Soviet_Union
gptkbp:firstIntroduced 1980s
gptkbp:fuelType contact and proximity fuses
gptkbp:futurePlans planned enhancements for accuracy and range
gptkbp:hasArea conducted in the 1980s
gptkbp:hasCapacity 1980s
gptkbp:hasFieldOfUse Tu-95,_Tu-160
gptkbp:hasVersion Kh-65E
https://www.w3.org/2000/01/rdf-schema#label Kh-65M
gptkbp:integration compatible with various aircraft
gptkbp:internationalRelations limited export to select countries
gptkbp:launched up to 45 degrees
gptkbp:launchSite strategic bombers
aircraft-mounted launchers
gptkbp:length 8.1 meters
gptkbp:manufacturer gptkb:Tactical_Missiles_Corporation
gptkbp:maxTakeoffWeight 2,900 kg
gptkbp:militaryRank gptkb:Gulf_War
gptkbp:modifications Kh-65M1, Kh-65M2
gptkbp:offers approximately $1 million
gptkbp:operationalArea anti-ship and land attack
gptkbp:operationalRange 300 km
gptkbp:operationalStatus in service
naval and land operations
gptkbp:productionCompany 1970s to 1980s
gptkbp:propulsion turbojet engine
gptkbp:provides active radar homing
inertial and terminal guidance
within 10 meters
gptkbp:providesGuidelinesFor inertial navigation system
gptkbp:range up to 300 km
gptkbp:safetyFeatures self-destruct mechanism
gptkbp:security low radar cross-section
reduces detection by radar
gptkbp:sensors active radar seeker
gptkbp:serviceHistory used in various conflicts
gptkbp:speed Mach_0.9
gptkbp:successor gptkb:Kh-101
gptkbp:supportRole varies by platform
high against stationary targets
gptkbp:targets land and naval targets
via radar or infrared
gptkbp:training requires specialized training for operators
gptkbp:type 600 kg
nuclear or conventional
gptkbp:usedBy gptkb:Russian_Armed_Forces
gptkbp:weight 2,900 kg
gptkbp:wingspan 3.2 meters