DocumentCode :
3205137
Title :
On the reliability of modular power conversion systems for small spacecraft
Author :
Schirone, Luigi ; Macellari, Michele ; Schiaratura, Alfiero
Author_Institution :
Dipt. di Ing. Aerospaziale e Astronautica, Univ. degli Studi di Roma La Sapienza, Rome
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
9
Abstract :
Modular power conversion systems for space application, thanks to their flexibility, can be easily adapted with minor changes to missions with different power requirements. In the perspective of an application to low-cost satellite, based on commercial off the shelf components, the main design drivers are efficiency and reliability. We will focus our attention to spacecrafts with body-mounted solar cells. Thus, trade-off between the opposite requirements, efficiency and reliability, have been discussed through the analysis of several redundancy schemes. Reliability calculation of circuits will be performed on the basis of MIL-HDBK-217F. The aim of this work is to demonstrate that specific design efforts allow to increase the reliability of COTS-based power systems to levels comparable to classical systems based on space qualified components.
Keywords :
artificial satellites; circuit reliability; power conversion; solar cells; space vehicle power plants; COTS-based power systems; MIL-HDBK-217F; body-mounted solar cells; low-cost satellite; modular power conversion system reliability; redundancy schemes; space application; spacecraft; Batteries; Industrial power systems; Photovoltaic cells; Power conversion; Power system analysis computing; Power system reliability; Redundancy; Satellites; Space missions; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839522
Filename :
4839522
Link To Document :
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