|
gptkbp:instanceOf
|
ballistic missile
|
|
gptkbp:decommissioned
|
gptkb:Russian_Federation
|
|
gptkbp:design
|
two-stage rocket
|
|
gptkbp:designatedAs
|
NATO_as_SS-4_Sandal
|
|
gptkbp:developedBy
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
1.2 meters
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:firstDeployment
|
1959
1980s
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:gameFeatures
|
liquid propellant
|
|
gptkbp:hasArea
|
Kapustin Yar
|
|
gptkbp:hasCapacity
|
1960
|
|
gptkbp:hasConflictWith
|
gptkb:Cuban_Missile_Crisis
|
|
gptkbp:historicalSignificance
|
Cold War deterrence
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-12 missile
|
|
gptkbp:influencedBy
|
V-2 rocket
|
|
gptkbp:internationalRelations
|
NATO-Soviet_tensions
|
|
gptkbp:launched
|
30 minutes
ground control
90 degrees
vertical launch
|
|
gptkbp:launchSite
|
mobile launcher
mobile launchers
|
|
gptkbp:length
|
8.4 meters
|
|
gptkbp:maxTakeoffWeight
|
4,000 kg
|
|
gptkbp:militaryRank
|
gptkb:Soviet_Army
|
|
gptkbp:numberBuilt
|
over 1,000
|
|
gptkbp:operationalRange
|
2,000 km
|
|
gptkbp:operationalStatus
|
decommissioned
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:productionCompany
|
1955-1959
|
|
gptkbp:provides
|
inertial navigation
inertial guidance
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:releaseRegion
|
gptkb:Eastern_Europe
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:retirementYear
|
1990
nuclear disarmament
nuclear arms reduction
|
|
gptkbp:serviceHistory
|
gptkb:Cold_War
|
|
gptkbp:status
|
decommissioned
|
|
gptkbp:strategicGoals
|
nuclear deterrent
|
|
gptkbp:successor
|
gptkb:R-14_missile
gptkb:R-14_Chusovaya
|
|
gptkbp:targets
|
1,000 meters
|
|
gptkbp:technology
|
ballistic missile technology
|
|
gptkbp:transportation
|
road transport
|
|
gptkbp:type
|
nuclear
1.0 megaton
|
|
gptkbp:usedBy
|
gptkb:Warsaw_Pact
|
|
gptkbp:weight
|
4,000 kg
|