|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:combat_radius
|
200 km
|
|
gptkbp:conflict
|
Cold War tensions
|
|
gptkbp:controls
|
gptkb:hospital
|
|
gptkbp:countermeasures
|
active jamming
|
|
gptkbp:country
|
limited export
|
|
gptkbp:date
|
1960s
|
|
gptkbp:deployment
|
aircraft carriers
air-to-air combat
|
|
gptkbp:design
|
high speed and agility
|
|
gptkbp:designed_by
|
gptkb:Monarch
|
|
gptkbp:developer
|
1960s to 1970s
|
|
gptkbp:diameter
|
0.35 meters
|
|
gptkbp:enemy
|
high-explosive
30 kg
|
|
gptkbp:engine_type
|
solid-fuel engine
|
|
gptkbp:exported_to
|
Warsaw Pact countries
|
|
gptkbp:features
|
aerodynamic shape
|
|
gptkbp:fighting_style
|
air superiority missions
|
|
gptkbp:filmography
|
air combat
air defense zones
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:guidance_system
|
semi-active radar homing
command guidance
within 5 meters
|
|
gptkbp:has_programs
|
Soviet missile program
|
|
gptkbp:historical_significance
|
part of Soviet military strategy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-4000 missile
|
|
gptkbp:integrates_with
|
with various aircraft systems
|
|
gptkbp:is_engaged_in
|
beyond visual range
|
|
gptkbp:is_tested_for
|
extensive flight tests
|
|
gptkbp:is_used_by
|
gptkb:Soviet_Air_Force
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
|
4.5 meters
4.0 meters
|
|
gptkbp:manufacturer
|
gptkb:Vympel
gptkb:Vympel_Design_Bureau
|
|
gptkbp:max_takeoff_weight
|
600 kg
200 kg
|
|
gptkbp:modifications
|
various upgrades
|
|
gptkbp:notable_battle
|
limited use in conflicts
|
|
gptkbp:notable_users
|
Warsaw Pact countries
|
|
gptkbp:operational_area
|
interceptor
|
|
gptkbp:operational_range
|
50 km
|
|
gptkbp:operational_status
|
obsolete
retired
|
|
gptkbp:origin
|
Soviet missile program
|
|
gptkbp:propulsion
|
solid rocket motor
|
|
gptkbp:provides_information_on
|
active radar homing
|
|
gptkbp:range
|
100 km
|
|
gptkbp:related_to
|
AAM-3 missile
|
|
gptkbp:retirement_year
|
1990s
advancements in missile technology
|
|
gptkbp:services
|
1970s
|
|
gptkbp:speed
|
Mach 2.5
|
|
gptkbp:status
|
retired
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:successor
|
gptkb:R-77_missile
R-77 development
K-13 missile
|
|
gptkbp:targets
|
gptkb:aircraft
radar lock-on
|
|
gptkbp:technology
|
missile guidance systems
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:weight
|
150 kg
500 kg
|
|
gptkbp:wingspan
|
2.5 meters
2.0 meters
|