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Application filed by Высокогорный геофизический институтfiledCriticalВысокогорный геофизический институт
Priority to SU4756507/23ApriorityCriticalpatent/SU1692243A1/en
Application grantedgrantedCritical
Publication of SU1692243A1publicationCriticalpatent/SU1692243A1/en
FIELD: meteorology. SUBSTANCE: anti-hail rocket has engine 1 with nozzle unit 2, head part 3 with safety system 4. Load compartment 5 is fitted with fins 6. Pyrotechnical slab 7 limited by partition 8 is located inside compartment 5. Time mechanism 9 with primer 10 is arranged between nozzle unit 2 and load compartment 5. Ignition case 11 is manufactured in the form of hollow screw with ignition holes 12. Sleeve 13 is fitted with folding blades 14. Disc containers 15 are closed by cover 16 embracing blades 14 and end of ignition case 11. Ejection charge 17 is placed in cover 16. EFFECT: enhanced functional efficiency of rocket by way of enlargement of its action zone on clouds. 4 dwg