EDePro AHR-EDePro-A6

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Rocket after launching from container

LAUNCHER CHARACTERISTICS

Caliber of container .........................60mm Caliber of rocket ..............................55mm No. of containers..............................6pcs Launcher weight ..............................65kg

Elevation range (50 incr.).................450÷850

Azimuth range (50 incr.) ..................00÷3600

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Usage of this anti-hail rocket system is simple and fast. Operator is qualified for handling with complete system within only a few hours of training. Rocket and container make unique system, which is placed on the launcher. Container represents launcher at the same time. Therefore, rocket is launched from its own container. This type of launching ensures great initial rocket speed (more than 80 m/sec.). Rocket containers are reusable. It is possible to launch rocket from different types of launchers, with only minimal modification on the launcher.

Rocket is almost completely made of thermoplastic materials, which do not pollute environment.

After the active phase of flight is finished (end of reagent discharge), rocket is self-destructed at safe altitude, while broken pieces, which are completely harmless, fall down. Right timing for activating the chain for rocket self-destruction are provided by two independent pyrotechnic timers.

The launcher enables the firing of single projectiles and salvo of rockets, and a swift exchange of containers. The dimensions of launcher are minimal, the construction compact and robust, and it has been designed so as to enable swift gaining of elevation and azimuth.

Antihail rocket A6 is in operational use world wide (Serbia, Bulgaria, Croatia, FYR Macedonia, Bosnia and Herzegovina, Argentina, etc.)

FUNCTIONAL CHARACTERISTICS OF ROCKET A6 Vertical range (elevation angle 850) .........................................5800 m Period of reagent emission.......................................................36* sec. Moment of self-destruction.......................................................43* sec. Operating temperature range for the rocket ....................... -20÷+60 0C Ignition circuit resistance............................................................. 1.2 Ω Required electricity for the activation ....................................... 0.68 A Required voltage ........................................................................... 24 V *Adjustable according to Users requirements.

GEOMETRIC AND MASS CHARACTERISTICS OF ROCKET A6

Caliber ........................................................................................55 mm Length .....................................................................................841 mm Mass ............................................................................................ 3.5 kg Center of gravity (measured from the rocket nose tip)............400 mm

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CONTAINER GEOMETRIC AND MASS CHARACTERISTICS Caliber ........................................................................................60 mm Length ....................................................................................1037 mm Mass ............................................................................................... 1 kg

REAGENT GENERATOR Start of discharge ........................................................................7* sec End of discharge........................................................................43* sec Reagent mass................................................................................ 400 g Reagent activity at -100C ........................................ 13105.2 ⋅ par/gmixture *Adjustable according to Users requirements.

Reagent generator cross section

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ROCKET MOTOR Propellant grain of main rocket motor is made of composite thermoplastic

propellant and inhibitor. Rocket grain configuration is star shaped with burning forehead surface. Combustion chamber is made of composites (glass-epoxide) while the nozzle material is glass-phenolic. Burning time ..............................................................................3.0 sec Motor total impulse.............................................................. 2150 Nsec Weight of propellant .................................................................. 1050 g

Rocket motor cross section

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EDePro Kralja Milutina 33 11000 Belgrade, Serbia, Europe Phone: +381 11 8064-380 Fax: +381 11 8064-940 E-mail: edepro@EUnet.rs All rights reserved by EDePro. Reprint in whole or in part not permitted.