|
gptkbp:instanceOf
|
air-to-air missile
|
|
gptkbp:controls
|
canard_control_surface
|
|
gptkbp:countermeasures
|
high resistance to flares
|
|
gptkbp:deployedTo
|
air superiority missions
ground attack missions
interception missions
defensive missions
offensive missions
|
|
gptkbp:designedBy
|
gptkb:Vympel
|
|
gptkbp:diameter
|
0.178 m
|
|
gptkbp:firstIntroduced
|
1973
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-73 family
|
|
gptkbp:launched
|
up to 90 degrees
|
|
gptkbp:launchSite
|
fighter aircraft
|
|
gptkbp:length
|
2.9 m
|
|
gptkbp:maxTakeoffWeight
|
120 kg
|
|
gptkbp:notableUsers
|
gptkb:China
gptkb:Egypt
gptkb:India
gptkb:Russia
gptkb:Syria
|
|
gptkbp:operationalRange
|
20 km
|
|
gptkbp:origin
|
gptkb:Soviet_Union
|
|
gptkbp:productionStartYear
|
1973
|
|
gptkbp:productionYears
|
present
|
|
gptkbp:propulsion
|
solid-fuel rocket motor
|
|
gptkbp:provides
|
active radar homing
semi-active laser guidance
infrared_homing
|
|
gptkbp:range
|
30 km
|
|
gptkbp:relatedPatent
|
gptkb:IRIS-T
ASRAAM
AIM-9 Sidewinder
AIM-132 ASRAAM
MICA
|
|
gptkbp:security
|
low radar cross-section
|
|
gptkbp:speed
|
Mach_2.5
|
|
gptkbp:successor
|
gptkb:R-74
|
|
gptkbp:supportRole
|
gptkb:Gulf_War
gptkb:Syrian_Civil_War
gptkb:Yugoslav_Wars
Ukraine_conflict
|
|
gptkbp:type
|
high-explosive
30 kg
|
|
gptkbp:variant
|
gptkb:R-73M2
gptkb:R-73M
R-73E
R-73M3
R-73M4
|
|
gptkbp:weight
|
105 kg
|
|
gptkbp:wingArea
|
four control fins
|
|
gptkbp:wingspan
|
1.8 m
|