|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:allows
|
limited range against high-speed targets
|
|
gptkbp:associated_with
|
gptkb:Monarch
|
|
gptkbp:challenges
|
technical difficulties
technological limitations of the era
|
|
gptkbp:combat_role
|
air defense
|
|
gptkbp:conflict
|
gptkb:Soviet-Afghan_War
|
|
gptkbp:controls
|
gptkb:rocket
R-3900 M
|
|
gptkbp:cultural_impact
|
depicted in media
|
|
gptkbp:decommissioned
|
gptkb:1995
gptkb:Russian_Federation
|
|
gptkbp:deployment
|
gptkb:1975
strategic deterrence
ground-based
|
|
gptkbp:design
|
engineers and scientists
defend against aerial threats
|
|
gptkbp:designed_by
|
gptkb:Monarch
|
|
gptkbp:developed_by
|
gptkb:Monarch
|
|
gptkbp:developer
|
gptkb:Soviet_Ministry_of_Defense
1960s to 1970s
|
|
gptkbp:diameter
|
1 meter
0.6 meters
|
|
gptkbp:enemy
|
high-explosive
nuclear
|
|
gptkbp:engine_type
|
gptkb:rocket
solid-fuel engine
|
|
gptkbp:exported_to
|
allied nations
|
|
gptkbp:features
|
modular design
high maneuverability
|
|
gptkbp:fighting_style
|
moderate
limited
|
|
gptkbp:filmography
|
gptkb:Eastern_Europe
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_type
|
kerosene and nitric acid
|
|
gptkbp:game_components
|
radar, launcher, missile
|
|
gptkbp:global_presence
|
non-proliferation treaty
|
|
gptkbp:guidance_system
|
gptkb:100_meters
semi-active radar homing
inertial guidance
|
|
gptkbp:historical_context
|
Soviet military strategy
|
|
gptkbp:historical_significance
|
Cold War era
part of Soviet air defense strategy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-3900 missile
|
|
gptkbp:influence
|
subsequent missile designs
|
|
gptkbp:influenced_by
|
earlier missile designs
|
|
gptkbp:is_aimed_at
|
terrestrial targets
|
|
gptkbp:is_countered_by
|
Warsaw Pact countries
|
|
gptkbp:is_integrated_with
|
integrated with radar systems
|
|
gptkbp:is_tested_for
|
gptkb:Kapustin_Yar
multiple
successful
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Armed_Forces
|
|
gptkbp:key
|
long range and high payload
|
|
gptkbp:launch_site
|
mobile launcher
mobile ground launcher
automated system
|
|
gptkbp:launched
|
vertical launch
|
|
gptkbp:legacy
|
influenced future missile designs
influenced missile technology
|
|
gptkbp:length
|
8.5 meters
10.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
gptkb:Vympel_Design_Bureau
|
|
gptkbp:max_takeoff_weight
|
3,200 kg
300 kg
|
|
gptkbp:notable_battle
|
gptkb:none
|
|
gptkbp:operational_area
|
strategic nuclear deterrent
|
|
gptkbp:operational_range
|
50 km
2,500 km
|
|
gptkbp:operational_status
|
obsolete
|
|
gptkbp:propulsion
|
solid rocket motor
liquid fuel
|
|
gptkbp:public_perception
|
strategic threat
|
|
gptkbp:range
|
50 km
2,500 km
|
|
gptkbp:related_to
|
R-300 missile system
|
|
gptkbp:research_and_development
|
ongoing until retirement
|
|
gptkbp:retirement_year
|
gptkb:1990
1990s
advancements in technology
technological obsolescence
replaced by more advanced systems
|
|
gptkbp:services
|
gptkb:1975
1970s
|
|
gptkbp:specifies
|
gptkb:market
|
|
gptkbp:speed
|
Mach 2.5
|
|
gptkbp:status
|
retired
decommissioned
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:strategic_importance
|
deterrent against NATO
|
|
gptkbp:successor
|
gptkb:R-400_missile
R-3900 M
R-400 missile system
|
|
gptkbp:targets
|
gptkb:radar_system
gptkb:aircraft
|
|
gptkbp:technology
|
missile guidance technology
|
|
gptkbp:training
|
crew training needed
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:weight
|
3,000 kg
300 kg
|
|
gptkbp:wingspan
|
3.5 meters
|