دورية أكاديمية

Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft

التفاصيل البيبلوغرافية
العنوان: Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft
المؤلفون: V. V. Ryzhkov, A. V. Sulinov
المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 4, Pp 115-128 (2018)
بيانات النشر: Samara National Research University, 2018.
سنة النشر: 2018
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: small and ultra-small spacecraft, propulsion systems, low-thrust rocket engines operating on various physical principles, total thrust impulse, specific thrust impulse, thrust, electric energy consumption, propulsion-system mass, spacecraft mass, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: The article presents an analysis of the possibility of using propulsion systems and rocket thrusters based on various physical principles and used as part of small and very small spacecraft. The parameters of efficient propulsion systems and low-thrust rocket engines are examined from the standpoint of being used as components of spacecraft fueled by various kinds of propellant: gaseous fuel, mono-fuel, including advanced compositions based on hydroxyl-ammonium nitrate, bipropellant fuel; xenon electric rocket systems, as well as special propulsion systems and low-thrust rocket engines operating on nitrous oxide, ammonia, gaseous hydrogen and oxygen; electric-powered systems based on pulsed plasma thrusters, ion and steady-state plasma engines. Taking into account the data analyzed, an attempt was made to categorize the propulsion systems and low-thrust rocket engines. Their use in small spacecraft, spacecraft of the Mini, Micro, Nano classes in various propulsion systems and low-thrust rocket engines was found to be preferable.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
Russian
تدمد: 2542-0453
2541-7533
Relation: https://journals.ssau.ru/vestnik/article/viewFile/6385/6266; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533
DOI: 10.18287/2541-7533-2018-17-4-115-128
URL الوصول: https://doaj.org/article/591e0e16dc6e4221b13142d7a62746ca
رقم الأكسشن: edsdoj.591e0e16dc6e4221b13142d7a62746ca
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:25420453
25417533
DOI:10.18287/2541-7533-2018-17-4-115-128