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Stability of a Rotating Spacecraft Partially Filled with Liquid: The Case of Several Cavities

机译：部分充满液体的旋转航天器的稳定性：多个腔的情况

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摘要

This paper is the second part of work and contains generalizations of the results of studying the stability of a rotating spacecraft with a cavity partially filled with liquid for the case of spacecraft with several cavities. These cavities can be embodied, first of all, by tanks containing liquid fuel components filling the tanks to a small depth. A particular example of spacecraft with two fuel tanks is considered. It is shown that the results obtained in [1], which relate to a rotating object with a single axisymmetric cavity of arbitrary configuration partially tilled (to a small depth) by low-viscosity liquid, admit generalization at rather natural limitations on an object with several cavities. When referring to formulas from [1], the latter are marked by superscript.
机译：本文是工作的第二部分，包含对带有多个空腔的航天器研究带有部分充满液体的空腔的旋转航天器的稳定性的研究结果的概括。这些腔首先可以通过容纳液体燃料成分的罐来实现，这些液体燃料成分填充到罐中的深度很小。考虑具有两个燃料箱的航天器的特定示例。结果表明，在[1]中获得的结果涉及具有任意构型的单个轴对称腔的旋转物体，该空腔由低粘度液体部分耕种（小深度），允许对具有以下特征的物体进行自然限制：几个腔。当引用[1]中的公式时，后者标有上标。

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