Statements (51)
Predicate | Object |
---|---|
gptkbp:instanceOf |
cruise missile
|
gptkbp:countermeasures |
active and passive countermeasures
|
gptkbp:deployedTo |
air-launched
|
gptkbp:design |
low-altitude flight profile
|
gptkbp:designedBy |
gptkb:Moscow_Institute_of_Thermal_Technology
|
gptkbp:developer |
significant investment
|
gptkbp:endurance |
limited by fuel capacity
|
gptkbp:exportedTo |
Soviet_Union_allies
|
gptkbp:firstFlight |
1979
conducted in the late 1970s |
gptkbp:firstIntroduced |
1980s
|
gptkbp:futurePlans |
planned enhancements for accuracy and range
|
https://www.w3.org/2000/01/rdf-schema#label |
Kh-59 missile
|
gptkbp:integration |
compatible with various aircraft
|
gptkbp:launched |
up to 45 degrees
single or salvo launch |
gptkbp:launchSite |
aircraft
aircraft-mounted launch system |
gptkbp:length |
8.0 m
|
gptkbp:manufacturer |
Raduga
|
gptkbp:maxTakeoffWeight |
1,000 kg
|
gptkbp:militaryRank |
enhanced strike capabilities for air forces
|
gptkbp:modifications |
Kh-59M,_Kh-59MK
|
gptkbp:notableUsers |
Russia,_India,_China
|
gptkbp:operationalRange |
300 km
|
gptkbp:operationalStatus |
in service
naval and land engagements |
gptkbp:productionCompany |
1970s to 1980s
|
gptkbp:propulsion |
turbojet engine
|
gptkbp:provides |
inertial and terminal guidance
inertial guidance with terminal active radar homing within 5 meters |
gptkbp:range |
up to 300 km
|
gptkbp:relatedTo |
gptkb:AGM-86_ALCM
|
gptkbp:security |
limited radar cross-section
designed to evade radar detection |
gptkbp:serviceHistory |
used in various conflicts
|
gptkbp:services |
approximately 15 years
|
gptkbp:speed |
0.8 Mach
|
gptkbp:strategicGoals |
precision strike capability
|
gptkbp:successor |
Kh-59M_missile
|
gptkbp:supportRole |
gptkb:Gulf_War
up to 1,000 km from base |
gptkbp:targets |
active radar homing
land and naval targets advanced radar targeting system |
gptkbp:type |
400 kg
high-explosive |
gptkbp:usedBy |
gptkb:Russian_Armed_Forces
|
gptkbp:weight |
1,000 kg
|
gptkbp:wingspan |
3.0 m
|