FIELD: rocket equipment; astronautics.
SUBSTANCE: invention can be used to reduce space rockets (SR) separating parts (SP) falling areas. In method of minimising SP exclusion zones extra heat required for combustion of SP in atmospheric part descent path to preset height, on which their combustion in atmosphere must end on is determined. Specific weight of power material is placed in a SP structure, for example, into cellular cells of shell nose cone structure.
EFFECT: reduced area of required exclusion.
1 cl
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