R-4  
Initial Operational Capability (IOC): 1961
Total Production: ?
Also Known As: AA-5 Ash, K-80, R-4M, R-4R and R-4T
Origin: Russia
Parent System: R-4
Initial Operational Capability (IOC): 1961
Total Production: ?
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Description: R-4, also known as the AA-5 Ash, was developed by the Soviet Union as an early medium range air-to-air missile for the Tu-128 air defense fighter/interceptor aircraft. As many other Soviet missiles R-4 was available equipped with a semi-active radar or infrared seeker.

R-4 Specifications

Dimensions
Diameter: 310 millimeter (12.2 inch)
Length: 5.30 meter (209 inch)
Wingspan: 1.30 meter (51 inch)
Performance
Max Range: 30,000 meter (16.2 nautical mile)
Speed
Top Speed: 475 mps (1,710 kph)
Weight
Weight: 390 kilogram (860 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total ?7
 
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