Solar energy harvesting on-board small satellites. (October 2020)

• Record Type: Journal Article
• Authors: Leverone, Fiona; Pini, Matteo; Cervone, Angelo; Gill, Eberhard
• Is Part Of: Renewable energy. Volume 159(2020)
• Page Start: 954
• Page End: 972
• Publication Date: 2020-10
• Subjects: Micro-ORC turbines -- Radial-inflow turbine -- Solar concentration -- Phase change material -- Optimisation; Renewable energy sources -- Periodicals; Power resources -- Periodicals; Énergies renouvelables -- Périodiques; Ressources énergétiques -- Périodiques; 333.794
• DOI: 10.1016/j.renene.2020.05.176
• Languages: English
• ISSNs: 0960-1481

Abstract

Abstract: 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%. Highlights: Feasibility of micro-organic Rankine cycles for space applications. Optimisation of a micro-ORC system from a size perspective. Highlights using a high-temperature phase change material for energy storage. Analysed the impact of turbine efficiency on the system design.