
1 - Fuze - head part; 2 - Ogive; 3 - Internal conical cap; 4 - Shaped charge liner (cumulative insert); 5 - Hollow charge; 6 - Insert; 7 - Fuze - bottom part; 8 - Mating ring; 9 - Pyrotechnic delay; 10 - Powder charge of rocket motor; 11 - Body of rocket motor; 12 - Fins; 13 - Shoe treads; 14 - Rocket jet; 15 - Coupling; 16 - Tracers; 17 - Cartridge case; 18 - Igniter; 19 - Propellant; 20 - Black powder in igniter; 21 - Electrical primer; 22 - Marking; 23 - The textile label with inscription; 24 -Index of manufacturer, series/year of production; 25 - Marking of projectile; 26 - Symbol of filling factory- series-year of production; 27 - Type of explosive; 28 - Series-year of completion - index of completing factory; 29 - Marking of projectile; 30 - Symbol of filling factory- series-year of production of rocket motor; 31 - Type of powder charge of rocket motor and symbol of factory- series-year of production of powder charge of rocket motor; 32 - Type of pyrotechnic timer; 33 - Symbol of factory- series-year of production of pyrotechnic timer; 34 - Type of tracers; 35 - Symbol of factory- series-year of production of tracers; 36 - Marking of cartridge case assembly; 37 - Type of propellant; 38 - Series-year and - index filling factory of powder; 39 - Series-year of production and symbol of filling factory; 40 - Weight of propellant; 41 - Index of manufacturer, series-year of production of head part projectile; 42 - Symbol of control; 43 - Index of manufacturer- series-year of production of head part projectile; 44 - Symbol of control; 45 - Symbol of filling factory- series-year of production of rocket engine; 46 - Symbol of the control; 47 - Symbol of control on the coercimeter.
73-PG-15V is used for engaging tanks, armoured vehicles, and self-propelled guns and against buildings and shelters. It is olive color with black text.
Complete round nomenclature is 73-PG-15V. Warhead nomenclature is PG-9. The rocket motor assembly nomenclature is PG-15P.
No information about functioning.
Fuze is VP-9.
Warhead contains A-IX-1, 0.322 kg.
Rocket motor contains Ngpp 0.6/7.5/90-11.8 (NBL-60), 0.16 kg.
Primer is EKV-23A.
Nothing else to see.