|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:controls
|
command and control systems
|
|
gptkbp:deployment
|
silo-based
|
|
gptkbp:design
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:developer
|
1955-1971
|
|
gptkbp:diameter
|
3 meters
3.0 meters
|
|
gptkbp:diplomatic_relations
|
gptkb:battle
up to 25 megatons
STARTI
|
|
gptkbp:enemy
|
gptkb:10
thermonuclear
|
|
gptkbp:engine
|
liquid-fueled
|
|
gptkbp:engine_type
|
RD-264
|
|
gptkbp:first_flight
|
gptkb:1966
gptkb:2018
|
|
gptkbp:first_introduced
|
gptkb:1971
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:has_ability
|
gptkb:1971
|
|
gptkbp:headcount
|
gptkb:10
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36 M
|
|
gptkbp:is_aimed_at
|
1,500 m
|
|
gptkbp:is_tested_for
|
over 100
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
gptkb:Hokage
automated
|
|
gptkbp:launched
|
silo launch
|
|
gptkbp:length
|
34.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:max_takeoff_weight
|
210,000 kg
|
|
gptkbp:membership
|
gptkb:SS-18_Satan
|
|
gptkbp:military_branch
|
gptkb:Strategic_Rocket_Forces
|
|
gptkbp:modifications
|
gptkb:R-36_M2
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
10,000 km
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
gptkb:item
|
|
gptkbp:provides_information_on
|
inertial
|
|
gptkbp:range
|
10,000 km
|
|
gptkbp:retired
|
gptkb:2018
|
|
gptkbp:retirement_year
|
gptkb:2018
|
|
gptkbp:seating_capacity
|
8,800 kg
|
|
gptkbp:service_history
|
gptkb:Monarch
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
limited
|
|
gptkbp:strategic_importance
|
deterrence
|
|
gptkbp:successor
|
gptkb:R-36_M2
gptkb:RS-28_Sarmat
|
|
gptkbp:type
|
gptkb:CEO
|
|
gptkbp:weight
|
210,000 kg
|
|
gptkbp:bfsParent
|
gptkb:R-36
gptkb:R-14_Chusovaya
|
|
gptkbp:bfsLayer
|
5
|