FIELD: weapon and ammunition.
SUBSTANCE: in the method of minimizing the exclusion zones for the detachable parts (DP) of the carrier rocket (CR) during the pre-flight preparation stage, the CR calculates the parameters of the motion of the DP before they fall to the ground. Based on the results of the calculations, the sections on the descent path for impact on the DP are determined, they form a signal in the process of an autonomous DP flight, and effect the design of the DP. The pyrotechnic composition is placed on the DP. During combustion, the pyrotechnic composition ensures heating of the DP to a temperature at which their combustion takes place in the incoming flow of atmospheric air, after reaching a height of 25-30 km, the ignition of the DP is carried out using an igniting composition.
EFFECT: maximum reduction of areas allocated for the areas of incidence of the DP CR.
6 cl, 1 tbl
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METHOD OF MINIMIZING EXCLUSION ZONES FOR CARRIER ROCKET DETACHABLE PARTS | 2018 |
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Authors
Dates
2017-08-01—Published
2015-09-01—Filed