Hsiung Feng II

GPTKB entity

Properties (59)
Predicate Object
gptkbp:instanceOf missile
gptkbp:countermeasures active and passive countermeasures
gptkbp:countryOfOrigin gptkb:Taiwan
gptkbp:deployedTo naval bases
gptkbp:design gptkb:Taiwan
modular design
anti-ship warfare
aerospace design
gptkbp:developedBy gptkb:National_Chung-Shan_Institute_of_Science_and_Technology
gptkbp:developer gptkb:National_Chung-Shan_Institute_of_Science_and_Technology
gptkbp:diameter 0.4 m
gptkbp:engineType turbojet engine
gptkbp:exportedTo not widely exported
gptkbp:firstFlight 1988
successful test flights
gptkbp:hasArea gptkb:Taiwan
operational testing
https://www.w3.org/2000/01/rdf-schema#label Hsiung Feng II
gptkbp:integration integrated with naval systems
gptkbp:internationalRelations limited international interest
gptkbp:launched vertical launch system
gptkbp:launchSite ship-based
ship-based launch system
gptkbp:launchVehicle ship-launched
gptkbp:length 6.5 m
gptkbp:manufacturer gptkb:National_Chung-Shan_Institute_of_Science_and_Technology
gptkbp:maxTakeoffWeight 600 kg
gptkbp:militaryRank navy
naval combat
deterrence strategy
enhanced naval capability
gptkbp:operationalRange 150 km
gptkbp:operationalRole anti-ship operations
gptkbp:operationalStatus operational
deployed on naval vessels
gptkbp:primaryUser gptkb:Republic_of_China_Navy
gptkbp:productionCompany 1980s
1980s to 1990s
gptkbp:propulsion turbojet engine
gptkbp:provides inertial and terminal guidance
inertial guidance system
gptkbp:range 150 km
gptkbp:researchAndDevelopment ongoing R&D efforts.
gptkbp:resources active radar homing
gptkbp:security limited radar cross-section
gptkbp:services 1990
gptkbp:speed subsonic
gptkbp:status in service
gptkbp:strategicGoals regional defense
gptkbp:successor gptkb:Hsiung_Feng_III
gptkbp:supportRole 150 km
naval warfare
high effectiveness against naval targets
gptkbp:targets surface ships
gptkbp:technology missile technology
gptkbp:type 300 kg
anti-ship missile
high-explosive warhead
gptkbp:weight 600 kg