In numbers Through the lens Video
NATO reporting name: AA-11 Archer
Letter “Ε” export version
The missile is designed to defeat air target (fighters, bombers, attack aircraft, airplane of military transport aviation) in a highly maneuverable close air combat round-the clock, from various aspects, against earth background and active enemy.
Technical specifications
| DESIGNER | NPO "Molniya", Research Institute of Electronic Devices (NIIEP) |
| COUNTRY | Russia |
| TYPE |
Short-range air-to-air missile
|
| Aircraft-bearer (aerial means) |
MiG-29, MiG-31, MiG-35, Su-24, Su-25, Su-33, Su-35, Su-57, Yak-130, J-10, HAL Tejas
|
|
POWER-PLANT
|
Solid - propellant rocket
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
2,9
|
|
Diameter, mm
|
0,200
|
|
Wing span, mm
|
0,500
|
|
Fin span, mm
|
-
|
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
105
|
| Warhead weight, kg |
8
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
2.655 |
|
Permissible (minimum) launch distance, m
|
- |
|
Target g-load, g
|
up to 12 |
|
Maximum launch range, km
|
|
|
- at the front hemisphere
|
30 |
|
- at the rear hemisphere
|
0,3 |
|
Caliber, mm
|
-
|
|
Fighter type target kill probability
|
- |
|
Guidance system
|
All-aspect, Infrared (IR) |
Photos R-77E Short-range air-to-air missile