Abstract
Efficiency of a hail suppression (HS) system is strongly affected technical devices in use, and the way they are used. In case of antihail actions, it is necessary to inject the meteorological reagent into the proper seeding area, as soon as possible. A technical description for the rocket TG-IO is given, together with theomethodology whichoi s base~ upon investigations of rocket operating in beams 25 wide, between -5 to -10 C isotherms on the front part of the Cb clouds.
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