Academic Journal

Selection of project structure for nanosatellite propulsion system

التفاصيل البيبلوغرافية
العنوان: Selection of project structure for nanosatellite propulsion system
المؤلفون: I. V. Belokonov, A. V. Ivliev, A. M. Bogatyrev, A. A. Kumarin, I. A. Lomaka, S. P. Simakov
المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 29-37 (2019)
بيانات النشر: Samara National Research University, 2019.
سنة النشر: 2019
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: nanosatellite, resistojet propulsion system, orbit correction, working fluid, thrust, flight prototype, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: This paper presents the results of theoretical and experimental research of a prototype of a propulsion system for periodical low-Earth orbit correction of research-and-educational nanosatellites. For that purpose, the prototype is to provide at least 20 m/s relative velocity for a 3U CubeSat with a mass not exceeding 4.5 kg. The personnel and environment safety were taken into account during testing and operation along with the ability to be launched as an associated payload by a “Soyuz”-series launch vehicle or from the ISS. An electro-thermal propulsion system (ResistoJet) was designed with “nonfreezing” mixture of ethanol and distilled water used as the working fluid. It is shown that a standard vehicle power system is capable of initiating one corrective thrust impulse per orbit with flight velocity change of about 0.1 m/s by introducing pulse energy storage units and allocating sufficient time for their charging in the flight profile. The propulsion system prototype was tested in atmospheric conditions. For that purpose shortened “atmospheric” nozzles were used. Testing was carried out using a zero-torque test-bench with high-speed cameras. The measured thrust value was in agreement with the calculated value of 44 mN.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
Russian
تدمد: 2542-0453
2541-7533
Relation: https://journals.ssau.ru/index.php/vestnik/article/view/7451; https://doaj.org/toc/2542-0453; https://doaj.org/toc/2541-7533
DOI: 10.18287/2541-7533-2019-18-3-29-37
URL الوصول: https://doaj.org/article/15fd862bdde64a32a2a1d694fe8ab83d
رقم الانضمام: edsdoj.15fd862bdde64a32a2a1d694fe8ab83d
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:25420453
25417533
DOI:10.18287/2541-7533-2019-18-3-29-37