|
gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:advances
|
ongoing modernization efforts
|
|
gptkbp:associated_systems
|
command and control systems
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:countermeasures
|
decoys and jammers
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:deployment
|
road-mobile
|
|
gptkbp:design
|
modular design
|
|
gptkbp:development
|
gptkb:1980s
|
|
gptkbp:diameter
|
3 meters
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:export_status
|
not exported
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:guidance_system
|
inertial guidance system
|
|
gptkbp:has_ability
|
high
|
|
gptkbp:has_units
|
over 300
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Topol-M
|
|
gptkbp:initial_deployment
|
gptkb:1997
|
|
gptkbp:inspiration
|
previous Soviet missile designs
|
|
gptkbp:integration_with_systems
|
integrated with early warning systems
|
|
gptkbp:international_status
|
strategic weapon
|
|
gptkbp:launch_control
|
mobile command post
|
|
gptkbp:launch_date
|
low frequency
|
|
gptkbp:launch_platform
|
mobile launcher
self-propelled launcher
|
|
gptkbp:launch_weight
|
47,200 kg
|
|
gptkbp:launch_window
|
vertical launch
|
|
gptkbp:length
|
22.7 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:military_branch
|
gptkb:Russian_Strategic_Rocket_Forces
|
|
gptkbp:nuclear_capable
|
gptkb:true
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_area
|
multiple launch regiments
|
|
gptkbp:operational_history
|
active since 1997
|
|
gptkbp:operational_range
|
11,000 km
|
|
gptkbp:partnerships
|
none known
|
|
gptkbp:payload_capacity
|
1,200 kg
|
|
gptkbp:propulsion
|
kerosene and liquid oxygen
|
|
gptkbp:range
|
11,000 km
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retirement_year
|
not retired
|
|
gptkbp:service_entry
|
gptkb:1997
|
|
gptkbp:speed
|
Mach 24
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
yes
|
|
gptkbp:stealth_technology
|
yes
|
|
gptkbp:strategic_importance
|
high
|
|
gptkbp:strategic_role
|
deterrence
|
|
gptkbp:successor
|
gptkb:RS-24_Yars
|
|
gptkbp:support_vehicles
|
transport vehicles
|
|
gptkbp:survivability
|
high
|
|
gptkbp:targeting_accuracy
|
300 meters
|
|
gptkbp:test_firing_location
|
gptkb:Kapustin_Yar
|
|
gptkbp:test_firing_years
|
1986-1997
|
|
gptkbp:testing_frequency
|
periodic testing
|
|
gptkbp:training_system
|
simulator training
|
|
gptkbp:warhead_type
|
thermonuclear
|
|
gptkbp:weight
|
47,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Strategic_Missile_Forces
gptkb:Strategic_Rocket_Forces
|
|
gptkbp:bfsLayer
|
5
|