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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:architectural_style
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gptkb:MKB_Raduga
|
|
gptkbp:controls
|
centralized
|
|
gptkbp:deployment
|
strategic missile forces
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:diplomatic_relations
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gptkb:battle
STARTI, STARTII
|
|
gptkbp:enemy
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gptkb:weapon
|
|
gptkbp:engine_type
|
RD-264
|
|
gptkbp:first_flight
|
gptkb:1966
successful
|
|
gptkbp:fuel_type
|
kerosene and nitric acid
|
|
gptkbp:guidance_system
|
1,500 meters
inertial guidance system
|
|
gptkbp:has_ability
|
gptkb:1971
|
|
gptkbp:has_programs
|
Soviet missile program
|
|
gptkbp:headcount
|
gptkb:10
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36 missile
|
|
gptkbp:is_tested_for
|
gptkb:2016
over 100
|
|
gptkbp:is_used_by
|
gptkb:Monarch
|
|
gptkbp:launch_site
|
mobile launcher
silos
automated system
|
|
gptkbp:launched
|
30 minutes
silo-based
|
|
gptkbp:legacy
|
one of the largest ICB Ms ever built.
|
|
gptkbp:length
|
34.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:max_takeoff_weight
|
210,000 kg
|
|
gptkbp:modifications
|
R-36 M, R-36 M2
|
|
gptkbp:notable_battle
|
gptkb:Monarch
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
up to 15,000 km
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
liquid propellant
|
|
gptkbp:range
|
10,000 km
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retired
|
gptkb:Russian_Federation
|
|
gptkbp:retirement_year
|
gptkb:2016
|
|
gptkbp:seating_capacity
|
up to 25 megatons
8,800 kg
|
|
gptkbp:services
|
gptkb:1970
|
|
gptkbp:speed
|
Mach 24
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
limited
|
|
gptkbp:strategic_importance
|
deterrence
|
|
gptkbp:successor
|
gptkb:R-36_M
|
|
gptkbp:survivability
|
high
|
|
gptkbp:transportation
|
rail and road
|
|
gptkbp:weight
|
210,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_K._Yangel
gptkb:R-14_Chusovaya
|
|
gptkbp:bfsLayer
|
5
|