gptkbp:instance_of
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gptkb:rocket
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gptkbp:associated_with
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gptkb:Monarch
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gptkbp:conflict
|
gptkb:Arab-Israeli_conflicts
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gptkbp:date
|
1949-1953
|
gptkbp:decommissioned
|
1990s
|
gptkbp:deployment
|
mobile and fixed sites
|
gptkbp:designated_as
|
NATO as SS-1 Scud
|
gptkbp:developed_by
|
gptkb:Monarch
|
gptkbp:diameter
|
0.88 m
|
gptkbp:enemy
|
nuclear or conventional
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gptkbp:engine_type
|
liquid-fueled engine
|
gptkbp:exported_to
|
several countries
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gptkbp:features
|
cylindrical body
|
gptkbp:fighting_style
|
limited combat use
|
gptkbp:first_flight
|
1953
|
gptkbp:guidance_system
|
1,000 m
inertial guidance
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gptkbp:historical_significance
|
early Soviet missile technology
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soviet R-17 Elbrus
|
gptkbp:influenced
|
subsequent missile systems
|
gptkbp:influenced_by
|
gptkb:German_V-2_rocket
|
gptkbp:is_tested_for
|
numerous test launches
|
gptkbp:is_used_by
|
gptkb:Warsaw_Pact
|
gptkbp:launch_site
|
mobile launcher
transportation erector launcher
|
gptkbp:launched
|
vertical launch
|
gptkbp:legacy
|
influenced modern missile design
|
gptkbp:length
|
8.4 m
|
gptkbp:manufacturer
|
gptkb:MKB_Raduga
|
gptkbp:max_takeoff_weight
|
3,000 kg
|
gptkbp:military_branch
|
gptkb:Soviet_Army
|
gptkbp:notable_event
|
used in conflicts
|
gptkbp:notable_features
|
high mobility
|
gptkbp:notable_users
|
gptkb:Politician
|
gptkbp:number_built
|
approximately 1,000
|
gptkbp:operational_area
|
gptkb:1955
limited operational use
|
gptkbp:operational_range
|
300 km
|
gptkbp:operational_status
|
retired from service
|
gptkbp:propulsion
|
kerosene and nitric acid
|
gptkbp:range
|
300 km
|
gptkbp:related_to
|
gptkb:Scud_missile
|
gptkbp:replaced_by
|
Tactical missile systems
|
gptkbp:retirement_year
|
1990s
|
gptkbp:role
|
tactical strike weapon
|
gptkbp:service_history
|
1955 to 1990s
|
gptkbp:status
|
retired
|
gptkbp:successor
|
R-300 Elbrus
|
gptkbp:weight
|
3,000 kg
|
gptkbp:wingspan
|
8.0 m
|
gptkbp:bfsParent
|
gptkb:North_Korean_Nodong_missile
|
gptkbp:bfsLayer
|
6
|