Solar energy harvesting on-board small satellites

RENEWABLE ENERGY

卷:159

Article

Leverone, Fiona^1,2  Pini, Matteo¹  Cervone, Angelo²  Gill, Eberhard² 

[1] Delft Univ Technol, Dept Prop & Power, Kluyverweg 1, NL-2629 HS Delft, Netherlands

[2] Delft Univ Technol, Dept Space Syst Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands

关键词: Micro-ORC turbines;    Radial-inflow turbine;    Solar concentration;    Phase change material;    Optimisation;   

DOI  :  10.1016/j.renene.2020.05.176

来源: Elsevier

【 摘 要 】

Small satellites are receiving increased recognition in the space domain due to their reduced associated launch costs and shorter lead time when compared to larger satellites. However, this advantage is often at the expense of mission capabilities, such as available electrical power and propulsion. A possible solution is to shift from the conventional solar photovoltaic and battery configuration to a micro-Organic Rankine Cycle (ORC) and thermal energy storage system that uses the waste energy from a solar thermal propulsion system. However, limited literature is available on micro-ORC systems, which are capable of producing a few hundred Watts of electrical power. This paper describes the proposed system layout and model of the integrated micro-ORC system, for various working fluids such as Toluene, Hexamethyldisiloxane (MM), and Octamethylcyclotetrasiloxane (D4). Toluene has been identified as a promising working fluid candidate resulting in a power generation system volume fraction of 18% for a 215 kg Low Earth Orbit satellite. The micro-ORC system is capable of producing 200 W of electrical power. The design provides high specific energies of at least 500 Wh/kg but, has a low shared specific power of 10 W/kg. A preliminary design of the micro-turbine provides a conservative total-to-static efficiency of 57%. (c) 2020 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).

【 授权许可】

Free