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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:allows
|
weather conditions affect performance
|
|
gptkbp:armament
|
gptkb:R-60_missile
|
|
gptkbp:challenges
|
technical difficulties during design
|
|
gptkbp:conflict
|
gptkb:Gulf_War
|
|
gptkbp:countermeasures
|
electronic countermeasures
|
|
gptkbp:deployment
|
gptkb:Monarch
Cold War era
|
|
gptkbp:designed_by
|
gptkb:Monarch
|
|
gptkbp:developer
|
1960s
1960s to 1970s
|
|
gptkbp:diameter
|
0.25 meters
|
|
gptkbp:diplomatic_relations
|
impact on arms control discussions
|
|
gptkbp:doctrine
|
air defense strategy
|
|
gptkbp:enemy
|
high-explosive
30 kg
|
|
gptkbp:exported_to
|
Warsaw Pact countries
|
|
gptkbp:features
|
aerodynamic shape
|
|
gptkbp:fighting_style
|
limited
air superiority missions
|
|
gptkbp:first_flight
|
gptkb:1965
gptkb:1967
|
|
gptkbp:guidance_system
|
high
active radar homing
semi-active radar homing
dual-mode guidance
|
|
gptkbp:historical_context
|
post-World War II military developments
|
|
gptkbp:historical_significance
|
Cold War missile technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-400 missile
|
|
gptkbp:integrates_with
|
aircraft systems
|
|
gptkbp:is_aimed_at
|
gptkb:aircraft
|
|
gptkbp:is_tested_for
|
ground and flight tests
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Air_Forces
|
|
gptkbp:launch_site
|
gptkb:aircraft
|
|
gptkbp:launched
|
up to 45 degrees
rail launcher
|
|
gptkbp:legacy
|
influenced future missile designs
|
|
gptkbp:length
|
3.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Vympel
gptkb:Vympel_Design_Bureau
|
|
gptkbp:max_takeoff_weight
|
200 kg
|
|
gptkbp:operational_area
|
defensive and offensive capabilities
|
|
gptkbp:operational_history
|
limited use in conflicts
|
|
gptkbp:operational_range
|
50 km
|
|
gptkbp:performance
|
high speed and agility
|
|
gptkbp:population_trend
|
shift towards guided munitions.
|
|
gptkbp:propulsion
|
solid rocket motor
|
|
gptkbp:provides_information_on
|
active radar homing
|
|
gptkbp:range
|
100 km
|
|
gptkbp:retirement_year
|
1990s
advancements in missile technology
|
|
gptkbp:safety_features
|
self-destruct mechanism
|
|
gptkbp:services
|
1970s
|
|
gptkbp:specifies
|
gptkb:market
|
|
gptkbp:speed
|
Mach 2.5
|
|
gptkbp:status
|
retired
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:strategic_importance
|
air superiority in military operations
|
|
gptkbp:successor
|
gptkb:R-77_missile
R-77 development
|
|
gptkbp:targets
|
gptkb:aircraft
active radar seeker
|
|
gptkbp:training
|
pilot training programs
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:wingspan
|
2.5 meters
1.5 meters
|