| 摘要 |
FIELD: aircraft; rocket engineering.SUBSTANCE: invention relates to rocket and aircraft equipment, and more specifically to attack unmanned systems for killing ground and water surface targets. In the fighting equipment (FE) compartment of an aircraft (AC), which involves a structural frame, a shell and an insert warhead (WH), the shell and the structural frame of the FE compartment are made from a structural material inflammable at blasting the WH and sustaining combustion in the air. In the structural frame there can be cavities, inside which there are ampoules with a liquid hydrocarbon or a solid thermobaric mixture for organization of deflagration combustion. In some cases, for example, if heat insulation of inner volumes of the FE compartment is needed, on the inner surface of the shell there may be heat-insulating mats installed, which are fixed on the shell pointly, with a pitch of not less than 10 mm. On the inner surface of the shell there may be a combustible composition applied with its ignition temperature of not less than the temperature of complete braking the air flow at maximum speed of the aircraft, but not more than ignition temperature of the shell structural material of the FE section. Combustible composition can be made heat-insulating. Between the WH and the shell there can be placed jettisonable in flight false targets, herewith the shell is made split.EFFECT: use of the proposed technical solution in unmanned attack AC will allow increasing fire power of the WH and incendiary action of the fighting equipment due to the synergetic effect of interaction the WH explosion products and the FE compartment elements, herewith in some cases there can be implemented an additional possibility to arrange in the FE compartment dropped in flight false targets.6 cl, 4 dwg |
