| 摘要 |
FIELD: military equipment, applicable in salvo-fire jet-propelled systems. ^ SUBSTANCE: the pin-stabilized rocket has a nose section with a liquid filler on the basis of petroleum products, and an air cavity, device fo0r scattering and ignition of the filler, rocket engine and a tail unit, in contrast to the prototype, according to the invention, the liquid filler in the rocket is positioned in a cylindrical body-tank made in the caliber of the rocket, whose center of inertia is removed relative to the center of inertia by no more than 8d, and the tail unit span makes up 0.2 to 0.4 of the value of removing of the center of inertia of the rocket, where d- the caliber of the rocket. ^ EFFECT: enhanced efficiency of fire injury. ^ 1 dwg |
