Special Production Plant "GAMRAT" Ltd.

POWDER ROCKET PROPELLANTS

ROCKET CHARGES

Rocket charges made from nitroglycerine powder of a ballistite type with an external diameter up to 130 mm, single- or multi-channel with the possibility of inhibiting the external surface.

Parameter:

calorific value within the range of 3500-4500 kJ/kg
linear burning speed 5-15 mm/s
specific impulse 1500-1700 N s/kg
density from 1,57-1,62 g/cm³

We produce in particular:

propulsion charges for aerial rocket missiles
propulsion charges for anti-tank rocket launchers
propulsion charges for anti-tank guided missiles
propulsion charges for rocket artillery

Propulsion charges for anti-tank rocket launchers

ARTILLERY NITROGLYCERINE TUBE POWDERS

Parameters:

thickness of the combustible layer 1,4 – 3,3 mm
calorific value 3200 kJ/kg
minimum density 1,54 g/³

We have a possibility of carrying out ballistic tests and we make ready-to-use charges with black powder.

MORTAR NITROGLYCERINE POWDERS

Parameters:

form of a band or discs
thickness of the combustible layer min 0,3 - 0,02 mm
calorific value max 5000 kJ/kg

HETEROGENEOUS ROCKET PROPELLANTS

Rocket propellants produced on the basis of liquid organic rubbers and inorganic oxidizers of perchlorate type with specific impulse of about 2400 Ns/kg and burning speeds formed by different catalytic systems. Charges are made by means of the vacuum casting method.

PYROTECHNICAL PRODUCTS

Various types of acoustic petards with a frictional or electrical fuse with an audibility range of 1,5-6 km.

Artillery shots simulators for Mss-7 launcher.

Explosive smoke grenades with infrared camouflage screening in visible band and in infrared with wavelength of 8-14 Om.










	POWDER ROCKET PROPELLANTS ROCKET CHARGES Rocket charges made from nitroglycerine powder of a ballistite type with an external diameter up to 130 mm, single- or multi-channel with the possibility of inhibiting the external surface. Parameter: calorific value within the range of 3500-4500 kJ/kg linear burning speed 5-15 mm/s specific impulse 1500-1700 N s/kg density from 1,57-1,62 g/cm³ We produce in particular: propulsion charges for aerial rocket missiles propulsion charges for anti-tank rocket launchers propulsion charges for anti-tank guided missiles propulsion charges for rocket artillery Propulsion charges for anti-tank rocket launchers ARTILLERY NITROGLYCERINE TUBE POWDERS Parameters: thickness of the combustible layer 1,4 – 3,3 mm calorific value 3200 kJ/kg minimum density 1,54 g/³ We have a possibility of carrying out ballistic tests and we make ready-to-use charges with black powder. MORTAR NITROGLYCERINE POWDERS Parameters: form of a band or discs thickness of the combustible layer min 0,3 - 0,02 mm calorific value max 5000 kJ/kg HETEROGENEOUS ROCKET PROPELLANTS Rocket propellants produced on the basis of liquid organic rubbers and inorganic oxidizers of perchlorate type with specific impulse of about 2400 Ns/kg and burning speeds formed by different catalytic systems. Charges are made by means of the vacuum casting method. PYROTECHNICAL PRODUCTS Various types of acoustic petards with a frictional or electrical fuse with an audibility range of 1,5-6 km. Artillery shots simulators for Mss-7 launcher. Explosive smoke grenades with infrared camouflage screening in visible band and in infrared with wavelength of 8-14 Om.
			polish version