INVESTIGATION OF THE EFFECTIVENESS OF THE USE OF CELLULAR PANELS IN THE SPACECRAFT BODY von Glazkov, I.E.

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METHOD OF CALCULATION OF LOADS OF THE PIPELINE FROM DYNAMIC INFLUENCES IN THE FLIGHT TIME OF THE LAUNCH VEHICLE von Glazkov, I.E., Filipov, A.G.

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EXPERIMENTAL IDENTIFICATION OF THE NONLINEAR DYNAMIC BEHAVIOR OF THE DESIGN OF A SMALL SPACE VEHICLE von Igolkin, A.A., Filipov, A.G., Balyaba, M.V., Glazkov, I.E.

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