DocumentCode
3088746
Title
Low Cost High Reliability Telemetry Module
Author
Abdelaziz, Aladin S. ; Mahmoud, Ahmed M. ; Yassen, Mohammed
Volume
0
fYear
2006
fDate
14-16 March 2006
Firstpage
1
Lastpage
8
Abstract
Satellites, their subsystems, and components are designed to meet specific reliability characteristics based on the desired life time of the satellite. Here in this paper I propose a specific reliability configuration for LEO small satellite telemetry module, its weight is around 3 Kg, and no failure probability (NFP) for the proposed design it was around 0.98 during the satellite mission of 3-years, and 0.95 till 5-years
Keywords
reliability; satellite telemetry; LEO small satellite telemetry module; reliability configuration; satellite mission; subsystem; Costs; Low earth orbit satellites; Redundancy; Reliability engineering; Remote sensing; Satellite broadcasting; Space technology; Switches; Telemetry; Temperature sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Radio Science Conference, 2006. NRSC 2006. Proceedings of the Twenty Third National
Conference_Location
Menoufiya
Print_ISBN
977-5031-84-2
Electronic_ISBN
977-5031-84-2
Type
conf
DOI
10.1109/NRSC.2006.386367
Filename
4275164
Link To Document