gptkbp:instanceOf
|
gptkb:spacecraft
|
gptkbp:currentStatus
|
in service
|
gptkbp:deployedTo
|
silo-based
|
gptkbp:design
|
gptkb:China
two-stage
|
gptkbp:designatedAs
|
NATO_as_CSS-4
|
gptkbp:diameter
|
3.35 meters
|
gptkbp:energyEfficiency
|
yes
up to 3 megatons
|
gptkbp:engineType
|
staged combustion cycle
|
gptkbp:firstFlight
|
1971
|
gptkbp:firstIntroduced
|
1981
|
gptkbp:fuelType
|
kerosene and nitric acid
|
gptkbp:gameFeatures
|
liquid
|
gptkbp:hasArea
|
multiple
12,000 km
|
gptkbp:headCoach
|
1
|
gptkbp:historicalSignificance
|
first Chinese ICBM
|
https://www.w3.org/2000/01/rdf-schema#label
|
China's DF-5
|
gptkbp:internationalCooperation
|
not_covered_by_INF_Treaty
|
gptkbp:launched
|
cold launch
|
gptkbp:launchSite
|
silo
|
gptkbp:length
|
32.6 meters
|
gptkbp:manufacturer
|
gptkb:China
|
gptkbp:maxTakeoffWeight
|
183,000 kg
|
gptkbp:militaryRank
|
gptkb:Rocket_Force
nuclear deterrence strategy
nuclear deterrence
|
gptkbp:numberBuilt
|
approximately 20
|
gptkbp:operationalRange
|
12,000 km
|
gptkbp:operationalStatus
|
active
silo-based
|
gptkbp:payloadCapacity
|
3,000 kg
|
gptkbp:productionCompany
|
1965
1965-1981
|
gptkbp:provides
|
1,000 meters
inertial
|
gptkbp:range
|
12,000 km
|
gptkbp:relatedPatent
|
DF-4
|
gptkbp:rival
|
gptkb:Soviet_R-36
|
gptkbp:serviceHistory
|
1981-present
|
gptkbp:speed
|
gptkb:Mach_24
|
gptkbp:status
|
in service
|
gptkbp:strategicGoals
|
yes
high
deterrence
|
gptkbp:successor
|
gptkb:DF-31
|
gptkbp:type
|
nuclear
liquid-fueled
|
gptkbp:usedBy
|
gptkb:People's_Liberation_Army_Rocket_Force
|
gptkbp:weight
|
183,000 kg
|