Mathematical model for the parametric study of ammonia propulsion system in microsatellite platform by random search method

• Main Authors: V. N. Blinov, A. I. Lukyanchik, V. V. Shalay
• Format: Article
• Language: English
• Published: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2018-10-01
• Series: Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
• Subjects: ammonia; correcting propulsion device; microsatellite; random search method; basic design parameters
• Online Access: https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2018/%D0%A2.%202,%20%E2%84%96%203/26-34%20%D0%91%D0%BB%D0%B8%D0%BD%D0%BE%D0%B2%20%D0%92.%20%D0%9D.,%20%D0%9B%D1%83%D0%BA%D1%8C%D1%8F%D0%BD%D1%87%D0%B8%D0%BA%20%D0%90.%20%D0%98.,%20%D0%A8%D0%B0%D0%BB%D0%B0%D0%B9%20%D0%92.%20%D0%92..pdf

A large number of basic design parameters of the ammonia propulsion system makes the task of their search by the method of random search urgent. The aim of the research is to create a mathematical model that is adapted to the chosen method. Mathematical model for random design parameters provides the choice of the optimal reduced mass of the propulsion system, taking into account the complex relationships of the investigated parameters, which provides the solution of the given tasks of microsatellite maneuvering