gptkbp:instance_of
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gptkb:rocket
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gptkbp:associated_with
|
gptkb:Monarch
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gptkbp:controls
|
R-29 RM
|
gptkbp:country
|
gptkb:Russia
|
gptkbp:deployment
|
gptkb:1976
strategic deterrence
|
gptkbp:design
|
strategic nuclear deterrence
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gptkbp:developed_by
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gptkb:Monarch
|
gptkbp:developer
|
1960s to 1970s
|
gptkbp:diameter
|
2.4 meters
|
gptkbp:enemy
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gptkb:weapon
|
gptkbp:engine_type
|
staged combustion cycle engine
|
gptkbp:features
|
multiple independently targetable reentry vehicles (MIR Vs)
|
gptkbp:filmography
|
gptkb:battle
|
gptkbp:first_flight
|
gptkb:1971
|
gptkbp:guidance_system
|
inertial guidance system
1,000 m CEP
|
gptkbp:historical_significance
|
part of Soviet nuclear triad
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-29 missile system
|
gptkbp:is_tested_for
|
numerous successful test launches
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gptkbp:launch_date
|
periodic test launches
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gptkbp:launch_site
|
gptkb:Dolphin-class_submarine
submarine command system
|
gptkbp:launched
|
vertical launch
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gptkbp:length
|
15.8 meters
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
gptkbp:max_takeoff_weight
|
40,000 kg
|
gptkbp:modifications
|
R-29 RM, R-29 RMU Sineva, R-29 RM U2 Layner
|
gptkbp:number_built
|
approximately 200
|
gptkbp:number_of_stages
|
gptkb:3
|
gptkbp:operational_area
|
gptkb:1976
|
gptkbp:operational_range
|
8,000 km
|
gptkbp:operational_status
|
active
|
gptkbp:primary_user
|
gptkb:Russian_Navy
|
gptkbp:propulsion
|
liquid propellant
|
gptkbp:range
|
8,000 km
Kura Test Range
|
gptkbp:retirement_year
|
still in service
|
gptkbp:safety_features
|
self-destruct mechanism
|
gptkbp:seating_capacity
|
up to 10 warheads
|
gptkbp:services
|
gptkb:1976
|
gptkbp:status
|
in service
in service with Russian Navy
|
gptkbp:strategic_importance
|
deterrent against nuclear attack
|
gptkbp:successor
|
gptkb:R-29_RMU_Sineva
R-29 RM U2 Layner
|
gptkbp:technology
|
ballistic missile technology
|
gptkbp:type
|
gptkb:rocket
|
gptkbp:weight
|
40,000 kg
|
gptkbp:bfsParent
|
gptkb:Mikhail_Yangel
|
gptkbp:bfsLayer
|
5
|