gptkbp:instance_of
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gptkb:rocket
|
gptkbp:architectural_style
|
OKB-586
|
gptkbp:conflict
|
gptkb:Monarch
|
gptkbp:deployment
|
1990s
Soviet strategic forces
|
gptkbp:design
|
strategic deterrence
deterrence through strength
|
gptkbp:developed_by
|
1960s
|
gptkbp:developer
|
1960s-1970s
|
gptkbp:diameter
|
3.0 meters
|
gptkbp:diplomatic_relations
|
gptkb:battle
STARTI
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gptkbp:enemy
|
up to 25 megatons
multiple independently targetable reentry vehicles (MIR Vs)
|
gptkbp:engine_type
|
RD-264
|
gptkbp:features
|
multiple warheads
|
gptkbp:first_flight
|
successful
|
gptkbp:first_introduced
|
gptkb:1971
|
gptkbp:fuel_type
|
kerosene and nitric acid
|
gptkbp:guidance_system
|
inertial guidance system
1,500 m CEP
|
gptkbp:historical_significance
|
symbol of Soviet military power
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36 M missile system
|
gptkbp:is_aimed_at
|
satellite guidance
|
gptkbp:is_tested_for
|
numerous
|
gptkbp:launch_date
|
low
|
gptkbp:launch_site
|
gptkb:Hokage
silo-based
automated system
|
gptkbp:legacy
|
one of the most powerful ICB Ms
|
gptkbp:length
|
34.3 meters
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
gptkbp:max_takeoff_weight
|
210,000 kg
|
gptkbp:military_branch
|
gptkb:Russian_Strategic_Rocket_Forces
|
gptkbp:notable_feature
|
heavy payload capacity
|
gptkbp:number_built
|
over 300
|
gptkbp:operational_area
|
gptkb:Central_Command
1971-1990s
|
gptkbp:operational_range
|
10,000 km
|
gptkbp:operational_status
|
decommissioned
|
gptkbp:origin
|
gptkb:Monarch
|
gptkbp:propulsion
|
liquid propellant
|
gptkbp:range
|
gptkb:Baikonur_Cosmodrome
10,000 km
|
gptkbp:retirement_year
|
1990s
arms reduction treaties
decommissioned in 1990s
|
gptkbp:service_branch
|
gptkb:Strategic_Rocket_Forces
|
gptkbp:speed
|
Mach 24
|
gptkbp:status
|
in service
|
gptkbp:strategic_importance
|
gptkb:weapon
high
|
gptkbp:successor
|
gptkb:R-36_M2
gptkb:RS-28_Sarmat
|
gptkbp:weight
|
210,000 kg
|
gptkbp:bfsParent
|
gptkb:Mikhail_Yangel
|
gptkbp:bfsLayer
|
5
|