|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:affiliatedWith
|
Soviet_missile_development_program
|
|
gptkbp:associatedWith
|
gptkb:Soviet_strategic_missile_forces
|
|
gptkbp:countryOfOrigin
|
gptkb:Soviet_Union
|
|
gptkbp:deployedTo
|
silo-based
|
|
gptkbp:design
|
large payload capacity
|
|
gptkbp:designatedAs
|
SS-18 Satan
|
|
gptkbp:diameter
|
3 meters
|
|
gptkbp:energyEfficiency
|
up to 25 megatons
|
|
gptkbp:engineType
|
RD-264
|
|
gptkbp:firstFlight
|
1966
2018
|
|
gptkbp:firstIntroduced
|
1971
|
|
gptkbp:gameFeatures
|
liquid propellant
|
|
gptkbp:hasArea
|
over 100
|
|
gptkbp:hasCapacity
|
1974
|
|
gptkbp:headCoach
|
10-14
|
|
gptkbp:historicalSignificance
|
one of the most powerful ICBMs
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36M
|
|
gptkbp:influenceOn
|
nuclear strategy
|
|
gptkbp:launched
|
automated launch control system
|
|
gptkbp:launchSite
|
silo
silo_launch_sites
|
|
gptkbp:legacy
|
influenced future missile designs
|
|
gptkbp:length
|
34.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
210,000 kg
|
|
gptkbp:modifications
|
gptkb:R-36M2
|
|
gptkbp:numberOfStudents
|
3
|
|
gptkbp:operationalRange
|
10,000 km
|
|
gptkbp:operationalStatus
|
active
strategic missile bases
|
|
gptkbp:payloadCapacity
|
8,000 kg
|
|
gptkbp:productionCompany
|
1960s to 1970s
|
|
gptkbp:provides
|
1,500 meters
inertial guidance system
|
|
gptkbp:range
|
10,000 km
|
|
gptkbp:retired
|
gptkb:Russian_Federation
|
|
gptkbp:retirementYear
|
2018
|
|
gptkbp:serviceHistory
|
gptkb:Cold_War
|
|
gptkbp:status
|
in service
|
|
gptkbp:strategicGoals
|
deterrence
|
|
gptkbp:successor
|
gptkb:RS-28_Sarmat
gptkb:R-36M2_Voevoda
|
|
gptkbp:technology
|
UR-100N
|
|
gptkbp:type
|
up to 10
multiple independently targetable reentry vehicles (MIRVs)
|
|
gptkbp:weight
|
210,000 kg
|