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Journal articles on the topic 'Propulsion électrique de satellite'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

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1

-KOPPEL, Christophe R. "Sous-systèmes de propulsion électrique pour satellites et sondes spatiales." Revue de l'Electricité et de l'Electronique -, no. 08 (2000): 71. http://dx.doi.org/10.3845/ree.2000.084.

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2

-Mazodier, Laurent. "La propulsion électrique des navires." Revue de l'Electricité et de l'Electronique -, no. 03 (1997): 30. http://dx.doi.org/10.3845/ree.1997.028.

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3

-GONDOUIN, D. "Nouvelles topologies de systèmes de propulsion électrique de navires." Revue de l'Electricité et de l'Electronique -, no. 09 (2000): 48. http://dx.doi.org/10.3845/ree.2000.090.

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4

Sabadosh, Lyubomyr, Serhii Larkov, Oleg Kravchenko, and Vladyslav Sereda. "Increasingly Safe, High-Energy Propulsion System for Nano-Satellites." Transactions on Aerospace Research 2018, no. 4 (2018): 38–44. http://dx.doi.org/10.2478/tar-2018-0028.

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Summary Numerous attempts have been undertaken to develop propulsion systems for nano-satellite-type spacecrafts to enable their maneuvering in orbits. One of the potentially viable chemical propellant propulsion systems is a hybrid system. The present paper studies propellant composition variants with the metal hydride as fuel that can be chosen for a nano-satellite hybrid propulsion system. It defines key requirements for chemical propellant nano-satellite propulsion systems, and specifies potential propellant pairs based on a compact metal hydride. The study describes basic technical charac

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5

Zaberchik, Michael, Dan R. Lev, Eviatar Edlerman, and Avner Kaidar. "Fabrication and Testing of the Cold Gas Propulsion System Flight Unit for the Adelis-SAMSON Nano-Satellites." Aerospace 6, no. 8 (2019): 91. http://dx.doi.org/10.3390/aerospace6080091.

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Adelis-SAMSON is a nano-satellite mission aimed at performing geo-location of target signals on Earth using a tight three-satellite formation in space. To maintain formation, each nano-satellite is equipped with a cold gas propulsion system. The design, qualification, and integration of the Adelis-SAMSON nano-satellite propulsion system is presented in this paper. The cold gas propulsion system mass is approximately 2 kg, takes a volume of 2U, and generates a thrust of 80 mN from four thrusters using krypton as a propellant. We first present the propulsion system requirements and corresponding

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6

Prickett, R. P., and J. V. Hoang. "Satellite propulsion performance modeling using flight data." Journal of Propulsion and Power 8, no. 5 (1992): 971–79. http://dx.doi.org/10.2514/3.23581.

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7

Sochacki, Mateusz, and Janusz Narkiewicz. "Propulsion System Modelling for Multi-Satellite Missions Performed by Nanosatellites." Transactions on Aerospace Research 2018, no. 4 (2018): 58–67. http://dx.doi.org/10.2478/tar-2018-0030.

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Abstract Progress in miniaturization of satellite components allows complex missions to be performed by small spacecraft. Growing interest in the small satellite sector has led to development of standards such as CubeSat, contributing to lower costs of satellite development and increasing their service competitiveness. Small satellites are seen now as a prospective replacement for conventional sized satellites in the future, providing also services for demanding users. New paradigms of multi-satellite missions such as fractionation and federalization also open up new prospects for applications

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8

-Michaux, Raymond. "Les machines discoïdes à champ axial dans les systèmes de propulsion électrique." Revue de l'Electricité et de l'Electronique -, no. 03 (1997): 37. http://dx.doi.org/10.3845/ree.1997.029.

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9

Wapman, Jonathan D., David C. Sternberg, Kevin Lo, Michael Wang, Laura Jones-Wilson, and Swati Mohan. "Jet Propulsion Laboratory Small Satellite Dynamics Testbed Planar Air-Bearing Propulsion System Characterization." Journal of Spacecraft and Rockets 58, no. 4 (2021): 954–71. http://dx.doi.org/10.2514/1.a34857.

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10

Khoucha, Farid, Abdelkhader Khoudiri, Mohamed EH Benbouzid, and Abdelaziz Kheloui. "Commande DTC d’une propulsion moteur asynchrone/onduleur multiniveau asymétrique pour un véhicule électrique." European Journal of Electrical Engineering 14, no. 2-3 (2011): 237–54. http://dx.doi.org/10.3166/ejee.14.237-254.

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11

Yang, An-Shik, and Tien-Chuan Kuo. "Design Analysis of a Satellite Hydrazine Propulsion System." Journal of Propulsion and Power 18, no. 2 (2002): 270–79. http://dx.doi.org/10.2514/2.5966.

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12

Kang, H. S. "Launch - Installation and Propulsion Control Satellite Locator System." IFAC Proceedings Volumes 33, no. 16 (2000): 161–66. http://dx.doi.org/10.1016/s1474-6670(17)39621-0.

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13

Soares Neto, T. G., J. Gobbo-Ferreira, A. J. G. Cobo, and G. M. Cruz. "Ir-Ru/Al2O3 catalysts used in satellite propulsion." Brazilian Journal of Chemical Engineering 20, no. 3 (2003): 273–82. http://dx.doi.org/10.1590/s0104-66322003000300007.

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14

NICULESCU, Filip, Constantin VALCU, Traian TIPA, Adrian SAVESCU, Mirela VASILE, and Constantin SANDU. "Measurement system for the parameters of satellite propulsion." INCAS BULLETIN 11, no. 3 (2019): 127–34. http://dx.doi.org/10.13111/2066-8201.2019.11.3.11.

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Within the STRAuSS (Advanced Solar Thermal Propulsion System for Increasing of Satellite Operational Life) project to investigate the extension of a satellite operation period, a new valve type and a new type of nozzle were designed. Extending the period of operation of the satellite propulsion is an important factor for increasing its activity period and reducing the production and launch costs. To measure the force generated when releasing propellant gas from the satellite reservoir, a dynamic fine-scale force measurement system has been designed. This system also measures experiment paramet

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15

KISARA, Katsuto, Hiroshi MIYAJIMA, and Kazuhiro NAKAHASHI. "Nozzle performance of bipropellant engines for satellite propulsion." Journal of the Japan Society for Aeronautical and Space Sciences 33, no. 373 (1985): 76–81. http://dx.doi.org/10.2322/jjsass1969.33.76.

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16

Ranjan, Ravi, S. K. Chou, Fahid Riaz, and Kumarasamy Karthikeyan. "Cold gas micro propulsion development for satellite application." Energy Procedia 143 (December 2017): 754–61. http://dx.doi.org/10.1016/j.egypro.2017.12.758.

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17

Lotfy, A., W. Anis, and Joseph V. M. Halim. "Design PV system for a small GEO satellite and studying the effect of using different types of propulsion." International Journal of Advances in Applied Sciences 8, no. 1 (2019): 54. http://dx.doi.org/10.11591/ijaas.v8.i1.pp54-63.

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<p>This paper presents an optimum design of the solar Photo-Voltaic (PV) power system for small Geostationary Earth Orbit (GEO) satellites using triple junction solar cells and advanced Lithium Ion batteries. The paper applies the proposed system on various propulsion technologies; full chemical, full electrical and hybrid propulsions. This research work studies the capability to fulfil efficiently all the satellite power requirements during both the launching and the on-station phases while reducing the high cost challenge. Since the propulsion type is a key factor for the satellite cos

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18

-LETELLIER, Paul. "Les machines à aimants permanents de grande puissance dans les systèmes de propulsion électrique." Revue de l'Electricité et de l'Electronique -, no. 09 (2000): 53. http://dx.doi.org/10.3845/ree.2000.091.

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19

Potrivitu, George-Cristian, Yufei Sun, Muhammad Wisnuh Aggriawan bin Rohaizat, et al. "A Review of Low-Power Electric Propulsion Research at the Space Propulsion Centre Singapore." Aerospace 7, no. 6 (2020): 67. http://dx.doi.org/10.3390/aerospace7060067.

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The age of space electric propulsion arrived and found the space exploration endeavors at a paradigm shift in the context of new space. Mega-constellations of small satellites on low-Earth orbit (LEO) are proposed by many emerging commercial actors. Naturally, the boom in the small satellite market drives the necessity of propulsion systems that are both power and fuel efficient and accommodate small form-factors. Most of the existing electric propulsion technologies have reached the maturity level and can be the prime choices to enable mission versatility for small satellite platforms in Eart

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20

Gagne, Kevin, M. McDevitt, and Darren Hitt. "A Dual Mode Propulsion System for Small Satellite Applications." Aerospace 5, no. 2 (2018): 52. http://dx.doi.org/10.3390/aerospace5020052.

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21

Kronhaus, Igal, and Klaus Schilling. "PICO-SATELLITE ORBIT AND ATTITUDE CONTROL BY ELECTRIC PROPULSION." IFAC Proceedings Volumes 46, no. 19 (2013): 277–82. http://dx.doi.org/10.3182/20130902-5-de-2040.00045.

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22

Lev, Dan R., Gregory D. Emsellem, and Ashley K. Hallock. "The Rise of the Electric Age for Satellite Propulsion." New Space 5, no. 1 (2017): 4–14. http://dx.doi.org/10.1089/space.2016.0020.

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23

OKAMOTO, Hirouyki, Mitsuteru SUGIKI, and Shin SATORI. "A3 Development of the Electric Propulsion for Small Satellite." Proceedings of the Space Engineering Conference 2002.10 (2002): 9–12. http://dx.doi.org/10.1299/jsmesec.2002.10.9.

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24

Savvas, Spiridon, Dimitrios Malamas, Alexandros Manoudis, et al. "Power Processing Unit For Micro Satellite Electric Propulsion System." E3S Web of Conferences 16 (2017): 15004. http://dx.doi.org/10.1051/e3sconf/20171615004.

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25

Guerrini, G., C. Michaut, M. Bacal, A. N. Vesselovzorov, and A. A. Pogorelov. "An intense Hall-type ion source for satellite propulsion." Review of Scientific Instruments 69, no. 2 (1998): 804–6. http://dx.doi.org/10.1063/1.1148572.

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26

Zhang, Wei, Jie Zhang, Huajun Chen, Bin Zhang, Feng Liu, and Jun Zhao. "Assembly Method for Satellite Propulsion System based on HoloLens." IOP Conference Series: Materials Science and Engineering 608 (August 27, 2019): 012035. http://dx.doi.org/10.1088/1757-899x/608/1/012035.

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27

Manente, M., F. Trezzolani, M. Magarotto, et al. "REGULUS: A propulsion platform to boost small satellite missions." Acta Astronautica 157 (April 2019): 241–49. http://dx.doi.org/10.1016/j.actaastro.2018.12.022.

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28

Pallichadath, V., L. Turmaine, A. Melaika, et al. "In-orbit micro-propulsion demonstrator for PICO-satellite applications." Acta Astronautica 165 (December 2019): 414–23. http://dx.doi.org/10.1016/j.actaastro.2019.09.004.

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29

Holdaway, R., Y. S. Wong, A. R. Martin, and P. M. Latham. "A reappraisal of satellite orbit raising by electric propulsion." Acta Astronautica 19, no. 6-7 (1989): 535–38. http://dx.doi.org/10.1016/0094-5765(89)90121-5.

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30

Li, Ze, and Tao Song. "Study on Mixture Ratio Control of Bipropellant Propulsion System on Satellite Based on Bypass Control System." Applied Mechanics and Materials 390 (August 2013): 338–42. http://dx.doi.org/10.4028/www.scientific.net/amm.390.338.

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Bipropellant propulsion system (MON-1MMH) provides motivation for orbit transfer, attitude control and station keeping, is mainly applied for GEO satellite. Most bipropellant propulsion systems of satellite do not have the ability to control mixture ratio of oxidizer and fuel. The primary function of bypass control system, as an important part of bipropellant propulsion system, is to control helium pressure in the propellant tanks in order to control mixture ratio. This paper researches adjustment of mixture ratio for bipropellant propulsion system. Mathematical model for key components in byp

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31

-LARS, Bertrand. "Quelle propulsion électrique pour des navires militaires de premier rang type frégate de 5000 tonnes ?" Revue de l'Electricité et de l'Electronique -, no. 03 (2006): 46. http://dx.doi.org/10.3845/ree.2006.030.

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32

Bartolo, Denis, and Cécile Cottin-Bizonne. "Matière active synthétique." Reflets de la physique, no. 57 (April 2018): 27–31. http://dx.doi.org/10.1051/refdp/201857027.

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Ces dix dernières années, la maîtrise des propriétés interfaciales d’objets micrométriques a permis la motorisation de robots colloïdaux, notamment par propulsion électrique ou électrochimique. Ces micronageurs artificiels se sont révélés capables de s’auto-organiser en de nouvelles classes de matériaux aux propriétés inattendues. Dans cet article, nous décrivons l’organisation originale de deux types de particules colloïdales autopropulsées : des colloïdes Janus non-attractifs exhibant un comportement collectif de type adhésif, et des colloïdes rouleurs (dits de Quincke) qui s’assemblent en d

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33

Sandu, Constantin, Valentin Silivestru, Grigore Cican, et al. "On a New Type of Combined Solar–Thermal/Cold Gas Propulsion System Used for LEO Satellite’s Attitude Control." Applied Sciences 10, no. 20 (2020): 7197. http://dx.doi.org/10.3390/app10207197.

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This paper presents the development, construction and testing of a new type of solar–thermal propulsion system which can be used for low earth orbit (LEO) satellites. Currently, the vast majority of LEO satellites are fitted with a cold gas propulsion system. Although such a propulsion system is preferred, the service duration of an LEO satellite is limited by the amount of cold gas they carry onboard. In the case of the new type of solar–thermal propulsion system proposed in this paper, the cold gas is first transferred from the main tank in a cylindrical service tank/buffer tank which is pla

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34

Byers, David C., and John W. Dankanich. "Geosynchronous-Earth-Orbit Communication Satellite Deliveries with Integrated Electric Propulsion." Journal of Propulsion and Power 24, no. 6 (2008): 1369–75. http://dx.doi.org/10.2514/1.35322.

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35

Harmansa, Nicholas-E., Georg Herdrich, Stefanos Fasoulas, and Ulrich Gotzig. "DEVELOPMENT OF A SATELLITE PROPULSION SYSTEM BASED ON WATER ELECTROLYSIS." International Journal of Energetic Materials and Chemical Propulsion 18, no. 3 (2019): 185–99. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.2019028538.

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36

Pierre, Jean-François. "Electric propulsion: a key to success in the satellite market." Air & Space Europe 1, no. 5-6 (1999): 21–22. http://dx.doi.org/10.1016/s1290-0958(00)88865-6.

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37

Fourie, Dan, Ian M. Hedgecock, Francesco De Simone, Elsie M. Sunderland, and Nicola Pirrone. "Are mercury emissions from satellite electric propulsion an environmental concern?" Environmental Research Letters 14, no. 12 (2019): 124021. http://dx.doi.org/10.1088/1748-9326/ab4b75.

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38

Xing, Yi, Mengyun Zhou, Tailin Xu, et al. "Core@Satellite Janus Nanomotors with pH‐Responsive Multi‐phoretic Propulsion." Angewandte Chemie 132, no. 34 (2020): 14474–78. http://dx.doi.org/10.1002/ange.202006421.

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39

Xing, Yi, Mengyun Zhou, Tailin Xu, et al. "Core@Satellite Janus Nanomotors with pH‐Responsive Multi‐phoretic Propulsion." Angewandte Chemie International Edition 59, no. 34 (2020): 14368–72. http://dx.doi.org/10.1002/anie.202006421.

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40

Blanes, Jose M., Ausias Garrigos, Jose A. Carrasco, et al. "Two-Stage MPPT Power Regulator for Satellite Electrical Propulsion System." IEEE Transactions on Aerospace and Electronic Systems 47, no. 3 (2011): 1617–30. http://dx.doi.org/10.1109/taes.2011.5937254.

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41

Han, Cho Young, Jae Ho You, Kyun Ho Lee, Hui Kyung Kim, and Sung Nam Lee. "Sensitivity analyses of satellite propulsion components with their thermal modelling." Advances in Space Research 47, no. 3 (2011): 466–79. http://dx.doi.org/10.1016/j.asr.2010.09.018.

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42

Miller, Sara, Mitchell L. R. Walker, Jack Agolli, and John Dankanich. "Correction: Survey and Performance Evaluation of Small- Satellite Propulsion Technologies." Journal of Spacecraft and Rockets 58, no. 4 (2021): 1. http://dx.doi.org/10.2514/1.a34774.c1.

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43

Lin, Zhen, and Yong Li. "Performance Analysis of Bipropellant Propulsion System on Special Working Conditions." Applied Mechanics and Materials 390 (August 2013): 296–300. http://dx.doi.org/10.4028/www.scientific.net/amm.390.296.

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At the end of a test satellite, oxidant of the propulsion system was exhausted ahead of fuel. Long-term monopropellant working condition without combustion, cool gas flow working condition and interim working condition were experienced, which trouble the de-orbit control of the satellite. In order to evaluate the performance of the propulsion system on the special working conditions during the satellite de-orbit, theoretic analysis of the specific thrusters is introduced. And effective calculation method is built. Based on the method and obtained remote data, the thrust and specific impulse of

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44

Somov, Ye I., S. A. Butyrin, and S. Ye Somov. "ADDITIONAL LAUNCHING AND APPROACH OF A SPACE ROBOT FOR SERVICING A GEOSTATIONARY SATELLITE." Izvestiya of Samara Scientific Center of the Russian Academy of Sciences 23, no. 2 (2021): 75–83. http://dx.doi.org/10.37313/1990-5378-2021-23-2-75-83.

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The problems of additional launching a space robot into a geostationary orbit and approaching a geostationary satellite for its maintenance are considered. The robot's attitude and orbit control system uses an electric propulsion unit, a propulsion system based on eight electric thermo-catalytic engines with pulse-width modulation of their thrust, and a gyro moment cluster based on four single-gimbal control moment gyroscopes (gyrodines). Numerical results are presented that demonstrate the effectiveness of the developed discrete guidance and control algorithms.

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45

-Lott, C. "Filtrage actif du réseau et lissage actif du couple à bord des navires à propulsion électrique." Revue de l'Electricité et de l'Electronique -, no. 03 (1997): 54. http://dx.doi.org/10.3845/ree.1997.032.

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46

Lian, Xiaobin, Jiafu Liu, Laohu Yuan, and Naigang Cui. "Mixed fault diagnosis scheme for satellite formation." Aircraft Engineering and Aerospace Technology 90, no. 2 (2018): 427–34. http://dx.doi.org/10.1108/aeat-11-2016-0206.

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Purpose The purpose of this paper is to present a solution for the uncertain fault with the propulsion subsystem of satellite formation, using the Lur’e differential inclusion linear state observers (DILSOs) and fuzzy wavelet neural network (FWNN) to perform fault detection and diagnosis. Design/methodology/approach The uncertain fault system cannot be described based on the accurate differential equations. The set-value mapping is introduced into the state equations to solve the problem of uncertainty, but it will cause output uncertainty. The problem can be solved by linearization of Lur’e d

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47

Chudoba, B., G. Coleman, L. Gonzalez, E. Haney, A. Oza, and V. Ricketts. "Orbital transfer vehicle (OTV) system sizing study for manned GEO satellite servicing." Aeronautical Journal 120, no. 1226 (2016): 573–99. http://dx.doi.org/10.1017/aer.2016.3.

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ABSTRACTIn an effort to quantify the feasibility of candidate space architectures for astronauts servicing Geosynchronous Earth Orbit (GEO) satellites, a conceptual assessment of architecture-concept and operations-technology combinations has been performed. The focus has been the development of a system with the capability to transfer payload to and from geostationary orbit. Two primary concepts of operations have been selected: (a) Direct insertion/re-entry (Concept of Operations 1 – CONOP 1); (b) Launch to low-earth orbit at Kennedy Space Center inclination angle with an orbital transfer to

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48

Khandekar, Pravin, Kanishka Biswas, Dushyant Kothari, and H. Muthurajan. "Nano Mechanical Properties of Ceramic Polymer Composite Micro Thruster Developed Using 3D Printing Technology." Advanced Science Letters 24, no. 8 (2018): 5884–90. http://dx.doi.org/10.1166/asl.2018.12214.

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Nano and micro satellites, when revolving around the earth, may drift by very small angle from their orbit. But this small angle drift may result in large deviation from their original orbit over a long distance which these satellite covers over a period of time. For the course correction of these satellites, very small thrust is required in specific direction. Normal propulsion system cannot serve this purpose, because the thrust may be too large for these satellites. That’s where the role of micro thrusters becomes important. These are MEMS devices which can produce very small thrust and can

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49

Mahmoud, Tarek, Saed Othman, A. Farrag, and Ahmed ELRaffiey. "ORBIT CONTROL USING ELECTRIC PROPULSION SYSTEMS FOR EARTH OBSERVATION SATELLITE SWARM." Journal of Al-Azhar University Engineering Sector 15, no. 55 (2020): 560–72. http://dx.doi.org/10.21608/auej.2020.87879.

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50

Soares, M. S., R. D. Barbosa, G. M. da Cruz, J. A. J. Rodrigues, and S. Ribeiro. "Effect of niobium addition in support catalysts applied in satellite propulsion." Materials Chemistry and Physics 189 (March 2017): 153–61. http://dx.doi.org/10.1016/j.matchemphys.2016.12.030.

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