Statements (55)
Predicate | Object |
---|---|
gptkbp:instanceOf |
air-to-air missile
|
gptkbp:controls |
digital flight control
|
gptkbp:countermeasures |
advanced algorithms
limited effectiveness against flares |
gptkbp:deployedTo |
air superiority missions
|
gptkbp:design_feature |
advanced aerodynamics
|
gptkbp:diameter |
0.178 meters
|
gptkbp:exportedTo |
several countries
|
gptkbp:firstFlight |
1989
|
gptkbp:futurePlans |
planned enhancements
|
gptkbp:hasArea |
extensive flight tests
|
gptkbp:hasExperienceIn |
limited
varies by aircraft high against maneuverable targets |
https://www.w3.org/2000/01/rdf-schema#label |
R-74 missile
|
gptkbp:integration |
various aircraft types
|
gptkbp:internationalRelations |
limited due to technology restrictions
Russia,_India,_China |
gptkbp:is_designed_to |
engaging aerial targets
|
gptkbp:launched |
up to 90 degrees
vertical or inclined |
gptkbp:launchSite |
airborne launch
|
gptkbp:length |
3.2 meters
|
gptkbp:manufacturer |
gptkb:Vympel
|
gptkbp:maxTakeoffWeight |
120 kg
|
gptkbp:missileSystem |
gptkb:R-73_family
gptkb:R-73_missile |
gptkbp:modifications |
several variants exist
|
gptkbp:operational_status |
gptkb:Russian_Air_Force
in service |
gptkbp:operationalRange |
20-40 km
|
gptkbp:origin |
gptkb:Russia
|
gptkbp:performance |
superior to earlier models
|
gptkbp:productionYears |
1980s to 1990s
|
gptkbp:propulsion |
solid-fuel rocket motor
|
gptkbp:provides |
high precision
active radar homing infrared_homing |
gptkbp:range |
up to 40 kilometers
|
gptkbp:releaseFormat |
fighter aircraft
|
gptkbp:releaseYear |
1994
|
gptkbp:safety_features |
low radar cross-section
|
gptkbp:serviceType |
1990s
|
gptkbp:speed |
gptkb:Mach_3.0
|
gptkbp:steering |
thrust vectoring
|
gptkbp:successor |
R-77 missile
|
gptkbp:targetMarket |
within seconds
|
gptkbp:targets |
heat signature
aircraft,_helicopters |
gptkbp:training |
pilot training required
|
gptkbp:type |
30 kg
high explosive |
gptkbp:weight |
105 kg
|
gptkbp:wingArea |
four control fins
|
gptkbp:wingspan |
0.8 meters
|