|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:associated_with
|
command and control systems
|
|
gptkbp:country
|
gptkb:Russia
|
|
gptkbp:date
|
1960s
|
|
gptkbp:deployment
|
strategic missile forces
|
|
gptkbp:developer
|
1960s to 1970s
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:diplomatic_relations
|
STARTI
|
|
gptkbp:enemy
|
multiple independently targetable reentry vehicles (MIR Vs)
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
RD-264
|
|
gptkbp:first_flight
|
gptkb:1973
over 30
|
|
gptkbp:guidance_system
|
1,500 meters
inertial guidance system
|
|
gptkbp:historical_significance
|
part of strategic nuclear triad
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-36 U2 missile system
|
|
gptkbp:influence
|
influenced later ICB Ms
|
|
gptkbp:innovation
|
liquid-fueled rocket technology
|
|
gptkbp:is_capable_of
|
gptkb:theorem
|
|
gptkbp:launch_site
|
Soviet missile silos
|
|
gptkbp:legacy
|
part of nuclear deterrent strategy
|
|
gptkbp:length
|
34.3 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:military_branch
|
gptkb:Russian_Strategic_Rocket_Forces
|
|
gptkbp:mode
|
silo-based
|
|
gptkbp:modifications
|
several variants
|
|
gptkbp:notable_feature
|
high payload capacity
|
|
gptkbp:operational_range
|
10,000 km
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:platform
|
silos
|
|
gptkbp:propulsion
|
liquid propellant
|
|
gptkbp:range
|
gptkb:Baikonur_Cosmodrome
10,000 km
|
|
gptkbp:retirement_year
|
1990s
treaty obligations
|
|
gptkbp:role
|
deterrence
|
|
gptkbp:seating_capacity
|
up to 10 warheads
|
|
gptkbp:service_history
|
gptkb:Monarch
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
limited
|
|
gptkbp:successor
|
gptkb:R-36_M2
gptkb:RS-24_Yars
|
|
gptkbp:weight
|
210,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_Yangel
|
|
gptkbp:bfsLayer
|
5
|