|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:architectural_style
|
gptkb:MKB_Raduga
|
|
gptkbp:armament
|
R-12 missile
|
|
gptkbp:controls
|
gptkb:auto_race
|
|
gptkbp:date
|
gptkb:1955
|
|
gptkbp:decommissioned
|
gptkb:1988
|
|
gptkbp:deployment
|
gptkb:1961
silo-based
|
|
gptkbp:developed_by
|
gptkb:Monarch
|
|
gptkbp:diameter
|
3.0 meters
|
|
gptkbp:enemy
|
nuclear
|
|
gptkbp:engine_type
|
RD-0105
|
|
gptkbp:features
|
two-stage
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_type
|
kerosene and nitric acid
|
|
gptkbp:guidance_system
|
1,500 m
inertial navigation
inertial guidance
|
|
gptkbp:has_programs
|
Soviet missile program
|
|
gptkbp:historical_significance
|
first Soviet ICBM
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-16 missile
|
|
gptkbp:influenced_by
|
gptkb:V-2_rocket
|
|
gptkbp:inspired_by
|
German missile technology
|
|
gptkbp:is_tested_for
|
multiple
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Armed_Forces
|
|
gptkbp:launch_site
|
mobile launcher
silos
|
|
gptkbp:launched
|
90 degrees
cold launch
|
|
gptkbp:legacy
|
paved the way for future ICB Ms
|
|
gptkbp:length
|
30.5 meters
|
|
gptkbp:max_takeoff_weight
|
120,000 kg
|
|
gptkbp:military_branch
|
gptkb:Strategic_Rocket_Forces
|
|
gptkbp:military_technology
|
strategic deterrence
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_area
|
gptkb:1960
|
|
gptkbp:operational_range
|
2,500 km
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
gptkb:item
100,000 N
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retirement_year
|
gptkb:1980
technological obsolescence
|
|
gptkbp:seating_capacity
|
1.5 megaton
|
|
gptkbp:service_history
|
1960-1980s
|
|
gptkbp:services
|
gptkb:1988
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:CEO
gptkb:R-36_missile
|
|
gptkbp:weight
|
120,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Mikhail_K._Yangel
|
|
gptkbp:bfsLayer
|
5
|