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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:architectural_style
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gptkb:MKB_Raduga
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gptkbp:associated_with
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gptkb:Dolphin-class_submarines
|
|
gptkbp:challenges
|
technological hurdles
|
|
gptkbp:controls
|
R-30 Bulava
R-29 RM U2 Layner
|
|
gptkbp:countermeasures
|
advanced countermeasures against interception
|
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gptkbp:country
|
gptkb:Russia
Soviet allies
|
|
gptkbp:decommissioned
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gptkb:Dolphin-class_submarines
|
|
gptkbp:deployment
|
gptkb:1976
strategic deterrence
|
|
gptkbp:design
|
reliability and accuracy
strategic nuclear deterrence
|
|
gptkbp:designed_by
|
gptkb:MKB_Raduga
|
|
gptkbp:developed_by
|
gptkb:Monarch
|
|
gptkbp:developer
|
1960s to 1970s
engineers and scientists
significant investment
|
|
gptkbp:diameter
|
1.5 meters
|
|
gptkbp:diplomatic_relations
|
capable of delivering nuclear payloads
|
|
gptkbp:doctrine
|
part of Russian military doctrine
|
|
gptkbp:enemy
|
gptkb:weapon
nuclear
up to 1.2 megatons
|
|
gptkbp:engine_type
|
staged combustion cycle engine
|
|
gptkbp:features
|
gptkb:aircraft
multiple warhead capability
|
|
gptkbp:first_flight
|
gptkb:1971
gptkb:1973
|
|
gptkbp:guidance_system
|
500 meters
1,000 meters
inertial guidance
inertial guidance system
|
|
gptkbp:has_programs
|
Soviet missile program
|
|
gptkbp:headcount
|
multiple warheads
|
|
gptkbp:historical_significance
|
gptkb:Monarch
symbol of military power
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-29 missile
|
|
gptkbp:influence
|
submarine warfare
|
|
gptkbp:is_aimed_at
|
terminal guidance
|
|
gptkbp:is_tested_for
|
gptkb:Kapustin_Yar
numerous
numerous successful test launches
operational testing
|
|
gptkbp:is_used_by
|
gptkb:Russian_Navy
gptkb:Soviet_Navy
|
|
gptkbp:launch_date
|
periodic testing and drills
|
|
gptkbp:launch_site
|
gptkb:submarine
gptkb:Dolphin-class_submarine
vertical launch system
submarine command
submarine command system
|
|
gptkbp:launched
|
vertical launch
up to 90 degrees
short launch preparation time
|
|
gptkbp:legacy
|
influenced future missile designs
|
|
gptkbp:length
|
15.8 meters
|
|
gptkbp:max_takeoff_weight
|
40,000 kg
|
|
gptkbp:mission
|
strategic capabilities
|
|
gptkbp:modifications
|
R-29 RM, R-29 RMU
R-29 R, R-29 RM
|
|
gptkbp:notable_battle
|
gptkb:none
|
|
gptkbp:number_built
|
over 300
|
|
gptkbp:operational_range
|
8,000 km
intercontinental
|
|
gptkbp:operational_status
|
decommissioned
active in service
|
|
gptkbp:propulsion
|
liquid fuel
liquid propellant
|
|
gptkbp:range
|
8,000 km
8300 kilometers
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:retirement_year
|
still in service
newer systems
|
|
gptkbp:role
|
part of the nuclear triad
|
|
gptkbp:safety_features
|
enhanced safety measures in design
|
|
gptkbp:seating_capacity
|
1,000 kg
|
|
gptkbp:service_history
|
1971 to present
|
|
gptkbp:services
|
gptkb:1971
gptkb:1976
2010s
|
|
gptkbp:speed
|
Mach 8
Mach 23
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
low radar cross-section
|
|
gptkbp:strategic_importance
|
gptkb:weapon
deterrent against nuclear threats
high for Russian military
|
|
gptkbp:successor
|
gptkb:R-29_RMU_Sineva
R-29 RMU
|
|
gptkbp:training
|
conducted regularly
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:weight
|
40,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_K._Yangel
|
|
gptkbp:bfsLayer
|
5
|