Super-capacitor energy storage for micro-satellites: Feasibility and potential mission applications

T Shimizu, C Underwood - Acta Astronautica, 2013 - Elsevier
Small satellites, weighting between 100 and 200kg, have witnessed increasing use for a
variety of space applications including remote sensing constellations and technology …

Sizing design and implementation of a flywheel energy storage system for space applications

K Aydin, MT Aydemir - Turkish Journal of Electrical …, 2016 - journals.tubitak.gov.tr
Flywheel energy storage systems have become an important research subject in recent
years. They are also considered for space applications instead of hazardous and bulky …

Design and implementation of a power distribution system adopting overcurrent protection

M Bekhti, M Bensaada, M Beldjehem - The Aeronautical Journal, 2020 - cambridge.org
One of the most critical aspects of a small satellite is the electrical power system (EPS) since
the electrical power is necessary for the satellite to operate correctly during its predefined …

Design and Qualification Tests of the Alsat-1 High Efficiency Solar Panels

B Mohammed - international journal of renewable energy research, 2013 - dergipark.org.tr
Since the commissioning of the manufacture facility and qualification of the processes in
2001, Alsat-1 solar panels were the first ones ever to be made and tested in house by SSTL …

A virtual instrument for the testing and performance evaluation of a microsatellite power supply system

C Zheng, KS Low - IEEE Transactions on Instrumentation and …, 2008 - ieeexplore.ieee.org
A multimission microsatellite is currently being built by the Satellite Engineering Centre,
Nanyang Technological University, Singapore, in collaboration with the DSO National …

[PDF][PDF] Effect of the bus voltage level on the power system design for microsatellites

M Bekhti, M Beldjehem, F Arezki - International Journal of Applied, 2022 - academia.edu
Each time there is a need for a satellite mission analysis, engineers need to coordinate
together the choice of one technology with regard to the other (ie solar cells technology …

Power subsystem of GÖKTÜRK 2 flight model

H Özkaya, E Akkuş, FE Karagöz… - 2013 6th International …, 2013 - ieeexplore.ieee.org
The purpose of a power subsystem is to ensure reliable delivery of electrical power
compatible with all loads under all foreseeable operational states and environments, during …

Power Subsystem of rasat flight model

H Özkaya, B Çolak, E İmre, BG Özdemir… - Proceedings of 5th …, 2011 - ieeexplore.ieee.org
The purpose of a power subsystem is to ensure reliable delivery of electrical power
compatible with all loads under all foreseeable operational states and environments, during …

BILSAT-1: First earth observation satellite of Turkey-Operations and lessons learned

G Yuksel, O Belce, H Urhan - Proceedings of 2nd International …, 2005 - ieeexplore.ieee.org
BILSAT-1 is an enhanced micro satellite designed and manufactured in the framework of a
KHTT program between SSTL (UK) and TUBITAK-BILTEN (Turkey). The satellite was …

Virtual instrument for a micro-satellite power supply system

KS Low, C Zheng - 2007 IEEE Instrumentation & Measurement …, 2007 - ieeexplore.ieee.org
A multi-mission micro-satellite is presently being built by the Satellite Engineering Centre,
Nanyang Technological University. Among the various sub-systems, the power supply is …