Evaluation of realization of limitation on booster attack and slip angle under action of various wind perturbation
Автор: Endutkina E.A.
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Механика и машиностроение
Статья в выпуске: 3-1 т.11, 2009 года.
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The article is dedicated to problems of guarantee of booster motion stability during flight in atmosphere. It is presented results of booster perturbed motion simulation under an action of various wind perturbations. It is carried out an evaluation of realization of limitation on booster attack (slip) angles by maximum velocity pressure. It is estimated restrictions for conditions of booster launch.
Booster, control system, wind perturbations, velocity pressure, attack (slip) angle, perturbed motion, motion simulation, aerodynamic characteristics, bending of the longitudinal axis, motion stability
Короткий адрес: https://sciup.org/148198584
IDR: 148198584
