|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:deployedTo
|
silo-based
|
|
gptkbp:design
|
nuclear deterrent
|
|
gptkbp:designatedAs
|
SS-18 Satan
|
|
gptkbp:diameter
|
3 meters
|
|
gptkbp:energyEfficiency
|
yes
up to 25 megatons
|
|
gptkbp:engineType
|
RD-264
|
|
gptkbp:firstDeployment
|
1988
|
|
gptkbp:firstFlight
|
1973
|
|
gptkbp:firstGeneration
|
2018
|
|
gptkbp:gameFeatures
|
liquid propellant
|
|
gptkbp:hasArea
|
2018
up to 10,000 km
|
|
gptkbp:historicalSignificance
|
significant
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36M2 Voevoda
|
|
gptkbp:internationalCooperation
|
START I
|
|
gptkbp:launched
|
low
automated control system
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
silos
vertical launch
|
|
gptkbp:length
|
34.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
210,000 kg
|
|
gptkbp:militaryRank
|
gptkb:Russian_Strategic_Rocket_Forces
deterrence strategy
|
|
gptkbp:modifications
|
R-36M2V
|
|
gptkbp:numberBuilt
|
approximately 50
|
|
gptkbp:operationalHistory
|
over 30 years
|
|
gptkbp:operationalRange
|
10,000 km
|
|
gptkbp:operationalStatus
|
gptkb:Soviet_Union
active
|
|
gptkbp:payloadCapacity
|
up to 8,000 kg
|
|
gptkbp:productionCompany
|
1960s to 1970s
|
|
gptkbp:provides
|
1,500 meters
inertial guidance system
|
|
gptkbp:range
|
10,000 km
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retirementYear
|
2018
phased out
|
|
gptkbp:services
|
1988
|
|
gptkbp:status
|
in service
|
|
gptkbp:strategicGoals
|
high
part of
deterrence
|
|
gptkbp:successor
|
gptkb:RS-28_Sarmat
R-36M3
|
|
gptkbp:team
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:type
|
multiple independently targetable reentry vehicles (MIRVs)
thermonuclear warhead
heavy ICBM
|
|
gptkbp:weight
|
210,000 kg
|