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UNGUIDED AVIATION ROCKET

C-8DM-BE

PURPOSE OF "S-8DM-BE" Unguided Aviation Rocket

The s-8DM-BE unguided aviation missile is of the "air-to-surface" class and is designed to destroy:

PURPOSE OF "S-8DM-BE" Unguided Aviation Rocket

The S-8DM-BE unguided air-to-surface missile is designed to destroy:

DEVICE OF THE S-8DM-BE ROCKET

Device The S-8DM-BE unguided aviation missile consists of a warhead, shelled with a solid volumetric detonating mixture, with a piezo-electric explosive device and a jet engine installed in it. The jet engine is a solid ballistic propellant and in the temperature range of 213 k to 333 k has the following characteristics: a total thrust impulse of 5394 N.s, to 5984 N.S; operating time from 0.45s to 1.3s. The warhead has a thermobaric action and upon detonation, a high-energy cloud is formed from the components of the bulk detonating mixture. In terms of high-explosive action, the explosion of the cloud is equivalent to the explosion of 5.5-6 kg of TNT. The detonator ensures safe operation during service handling of the missile and reliable action on impact and on any type of surface, even with ricochet angles of meeting the target.

CALIBER, mm
80
LENGTH, mm
1615 max
MASS, kg OF <BR> THE ROCKET
11,6
MASS, kg OF <BR> THE COMBAT PART
3,8
MASS, kg OF<BR> THE VOLUME <BR>DETONATING <BR>MIXTURE
2,15
MAXIMUM <BR> PROPER <BR>SPEED, m/s
590
TNT EQUIVALENT, <BR>kg TNT
5,5:9
SHOOT <BR>DISTANCE, m
1300:4000
TEMPERATURE <BR>RANGE OF <BR>COMBAT USE,<BR> K(°C)<BR><BR>
FROM 213 TO 333 <BR> (-60 до+60)
PROBABLE<BR> DEVIATION OF <BR>TECHNICAL <BR> DISPERSION <BR>OF MISSILES <BR> FIRED FROM<BR> AIRCRAFT, MRAD
3
PROBABLE <BR> TECHNICAL <BR>DISPERSION <BR>DEVIATION <BR>OF MISSILES <BR>FIRED FROM <BR>HELICOPTER,<BR> MRAD
8
CALIBER, mm
LENGTH, mm
MASS, kg OF THE ROCKET
MASS, kg OF THE COMBAT PART
MASS, kg OF THE VOLUME DETONATING MIXTURE
MAXIMUM PROPER SPEED, m/s
TNT EQUIVALENT, kg TNT
SHOOT DISTANCE, m
TEMPERATURE RANGE OF COMBAT USE, K(°C)<BR><BR>
PROBABLE DEVIATION OF TECHNICAL DISPERSION <BR>OF MISSILES FIRED FROM AIRCRAFT, MRAD
PROBABLE TECHNICAL DISPERSION DEVIATION <BR>OF MISSILES FIRED FROM HELICOPTER, MRAD
80
1615 max
11,6
3,8
2,15
590
5,5:9
1300:4000
FROM 213 TO 333 <BR> (-60 до+60)
3<BR><BR>
8

UNGUIDED AVIATION ROCKET "C-8DM-BE"

With thermobaric action. In the center of the explosion, it creates an overpressure, in the order of 2.9MPa and a temperature above 28009C. Explosive device FPZ-17TV Piezoelectric, duplicated with inertial action. Safety type, with remote winding provided by clock mechanisms unaffected by weather conditions. With electronic protection from non-standard situations during flight.

List of carriers The S-8DM-BE unguided aviation missile is included in the armament of Russian-made aircraft and helicopters.

Shooting with the unguided C-8DM-BE air missile is carried out by: - ​​20 B-8 trunk blocks and its modifications B-8-0, B-8M and B-8MI, mounted on front-line and naval aviation aircraft. - 20 trunk blocks B-8B20-A, suspended on combat helicopters. - 7-barrel blocks B-8B7 and B-8C7.

Unguided aviation missiles are stored in wooden packages in indoor warehouses. In field conditions, they are stored under sheds or tarpaulins, excluding direct exposure to moisture and sunlight. The S-8DM-BE unguided aviation missiles are transported in their packaging by all types of transport.

Unguided aviation missile C-8DM-BE: 4 pcs. in a wooden case;

Package dimensions, mm: 1770x300x275

Volume m3: 0.146

Gross mass, kg: 70

Hazard Class: 1.1.F

UN: 0180

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