In numbers Through the lens Video
Test start: 2016
First appearance: at war in Syria, the 2019
First presentation: 2021 static exhibition “Army-2021”
Adoption into service: 2022
Helicopter's - bearer: Mi-28NM, Ka-52M και Mi-8AMTSh-VM “Sapsan”
Acronym LMUR: Light multipurpose guided missile
Letter “E” – export version
Other names: izdeliye 305 and izdeliye 305E
Izdeliye 305E missile is designed for round-the-clock engagement of single/group, moving/stationary, ground/above-water heat-contrast objects and covered/open enemy's manpower. The missile is designed on a "fire-and-forget" basis.
| Training missiles |
 |
| 305E-UL light training missile. |
 |
| Mockup 305E-Maket. |
Technical specifications
| DESIGNER | JSC “RPC “KBM” |
| COUNTRY | Russia |
| TYPE |
Air-to-surface missile
|
| Helicopter's-bearer (aerial means) |
Mi-28NM, Ka-52M and Mi-8AMTSh-VM “Sapsan”
|
|
POWER-PLANT
|
Rocket engine
|
|
Thrust, kgf
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
1,945
|
|
Diameter, m
|
0,20
|
|
Wing span, m
|
-
|
|
Fin span, m
|
-
|
|
WEIGHT
|
|
|
Maximum missile weight, kg
|
105
|
| Warhead weight, kg |
25
|
|
PERFORMANCE
|
|
|
Maximum speed, m/s (km/h)
|
until 230 (828) |
|
Missile flight altitude, m
|
100-600 |
|
Guided flight range (guaranteed), km
|
14,5 |
|
Operation temperature range, oC
|
-50.....+50 |
|
Seeker
|
Optical thermal-imaging |
|
Warhead type
|
blast-fragmentation |
|
Guidance system
|
|
| Combined with | inertial guidance with correction from satellite navigation equipment and self-guidance under control of seeker with ability to involve operator on the terminal part of trajectory. |