FIELD: weapons and ammunition.
SUBSTANCE: controlled aviation bomb comprises body and detachable yokes for fixation of solid-propellant rocket engine to bomb body. Yokes are arranged with the possibility for fixation of rocket engines of various capacity and comprises device for separation of engine from bomb in process of flight. Device for engine separation is connected to system of homing and control. It is preferable to make yokes from two halves, which cover bomb body and are tightened to each other by means of pyropushers. It is also preferable to equip the rocket engine with indicator of pressure reduction in engine chamber, connected to system of homing and control. System of homing and control may be provided with the unit that generates and distributes command for actuation of pyropushers as per specified time.
EFFECT: invention provides for the possibility to replace rocket engine for variation of application range in process of operation depending on urgent tasks.
6 cl, 3 dwg
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Authors
Dates
2010-06-10—Published
2008-08-29—Filed