Work

Energy Storage Selection for LEO Satellites

Year: 2013

Type: article

Abstract: This paper presents two energy storage systems, based on chemical batteries and flywheels as the energy source of low earth orbit satellites in eclipse duration.Each system is designed and optimized with regard to energy requirement of a typical LEO satellite and various vital parameters in satellites which are discussed.The storage system and electronic interface are presented to give an adequate view for comparing them in different aspects.Afterwards, a comparison between these energy storage systems (ESSs) is applied considering their efficiency, reliability, weight, operational temperature and self-discharge dissipation (trickle charge).Finally, the conclusion presents the most recommended system in order of their capability.

Source: International Journal of Machine Learning and Computing

DOI: 10.7763/ijmlc.2013.v3.322

Authors: B. Abdi, A. Alimardani, R. Ghasemi, S. M. M. Mirtalaei

Institutions: Islamic Azad University, Tehran, Amirkabir University of Technology, Islamic Azad University of Damavand

Language: English

Topic: Spacecraft Design and Technology

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: bronze

OpenAlex ID: W2319590269