|
gptkbp:instanceOf
|
missile
|
|
gptkbp:construction_cost
|
classified
|
|
gptkbp:deployedTo
|
gptkb:Republic_of_China_Navy
1980s
|
|
gptkbp:design
|
aerial warfare
|
|
gptkbp:developer
|
gptkb:Taiwanese_military
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:exportedTo
|
no known exports
|
|
gptkbp:firstFlight
|
1980
|
|
gptkbp:hasArea
|
successful test flights
|
|
gptkbp:hasExperienceIn
|
not used in combat
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hsiung Feng I
|
|
gptkbp:influence
|
modern missile technology
|
|
gptkbp:launchSite
|
vertical launch system
|
|
gptkbp:length
|
6.5 m
|
|
gptkbp:manufacturer
|
gptkb:National_Chung-Shan_Institute_of_Science_and_Technology
|
|
gptkbp:militaryRank
|
regional security
|
|
gptkbp:militaryService
|
naval forces
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operationalRange
|
150 km
|
|
gptkbp:origin
|
gptkb:Taiwan
|
|
gptkbp:productionYears
|
1970s to 1980s
|
|
gptkbp:propulsion
|
turbojet engine
|
|
gptkbp:provides
|
inertial guidance system
|
|
gptkbp:range
|
150 km
|
|
gptkbp:releaseFormat
|
ship-based
|
|
gptkbp:resources
|
active radar homing
|
|
gptkbp:retirementYear
|
2000s
|
|
gptkbp:serviceType
|
1980s
|
|
gptkbp:speed
|
subsonic
|
|
gptkbp:strategicGoals
|
deterrence
|
|
gptkbp:successor
|
gptkb:Hsiung_Feng_II
gptkb:Hsiung_Feng_III
improved range and guidance
|
|
gptkbp:targets
|
naval vessels
surface ships
|
|
gptkbp:team
|
Taiwanese_engineers
|
|
gptkbp:technology
|
gptkb:Hsiung_Feng_II
|
|
gptkbp:type
|
anti-ship missile
high-explosive warhead
|
|
gptkbp:weight
|
1,200 kg
|