Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite

This paper presents the multidisciplinary design optimization of monopropellant propulsion system of the nanosatellite for planner maneuver. Mass, configuration and internal ballistic equations are derived for any part of propulsion system (thruster, tank, pressurized gas, ...). Minimizing total mas...

詳細記述

書誌詳細

出版年:	فصلنامه علوم و فناوری فضایی
主要な著者:	M. Nosratollahi, A. h. Adami-Dehkordi
フォーマット:	論文
言語:	ペルシア語
出版事項:	Aerospace Research Institute 2011-01-01
主題:	monopropellant propulsion system multidisciplinary design optimization (mdo) space maneuver nanosatellite
オンライン･アクセス:	https://jsst.ias.ir/article_14405_4058a10a6a6af5d77276b5fede55ddef.pdf