In numbers Through the lens Video
NATO reporting name: AA-5 Ash
Αlso known as: K-80
Technical specifications
| DESIGNER | "Vympel" Design buream |
| COUNTRY | Russia |
| TYPE |
Medium range air-to-air missile
|
| Aircraft-bearer (aerial means) |
Tu-128M, Tu-128S-4
|
|
POWER-PLANT
|
Solid fuel booster rocket engine
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
|
|
- R-4R
|
5,3
|
|
- R-4T
|
5,23
|
|
Diameter, m
|
0,310
|
|
Wing span, m
|
|
|
- R-4R
|
1,550
|
|
- R-4T
|
1,227
|
|
Fin span, m
|
|
|
- R-4R
|
1,320
|
|
- R-4T
|
0,674
|
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
460
|
|
- R-4R
|
492
|
|
- R-4T
|
512
|
|
Warhead weight, kg
|
|
|
- R-4R
|
53,5
|
|
- R-4T
|
53,3
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
1.752 |
|
Target g-load, g
|
- |
|
Flight altitude, km
|
- |
|
Maximum launch range, km
|
|
|
- R-4R
|
30
|
|
- R-4T
|
15
|
|
Caliber, mm
|
-
|
|
Warhead type
|
High-explosive |
|
Target capture, flying at supersonic speeds, km/h
|
2.000 / 2.500 |
|
Fighter type target kill probability
|
- |
|
Guidance system
|
|
|
- R-4R
|
Semiactive radar
|
|
- R-4T
|
Infrared (ΙR)
|