Research of maneuverable possibilities of orbit plane at descent in atmosphere in contingencies

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The maneuverable possibilities of an orbit plane are researched at a descent in atmosphere in contingencies, connected with an extinction of its deduction into Earth satellite orbit. The areas of an accessibility and area of probable hit with satisfaction of limitations on control, conditions of driving in atmosphere and terminal conditions are calculated.

Короткий адрес: https://sciup.org/148197583

IDR: 148197583

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