Analytical Estimates of the Motion and Elastic Vibrations of the Structures of Separated Fairing Flaps of Rocket-Space Systems

Equations are obtained, and a model is constructed for studying the dynamics of separation of fairing flaps of rocket and space systems. Based on the assumption that the angular velocity of rotation of fairing flaps during separation is small compared to the lower frequencies of their natural vibrat...

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Veröffentlicht in:	Doklady. a journal of the Russian Academy of Sciences. Physics 2021-05, Vol.66 (5), p.134-138
Hauptverfasser:	Bakulin, V. N., Borzykh, S. V.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engines Angular velocity Classical Mechanics Estimates Launch vehicles Mathematical analysis Mathematical and Computational Physics Mathematical models Mechanics Physics Physics and Astronomy Rocket engines Separation Theoretical
Online-Zugang:	Volltext
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