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http://dx.doi.org/10.5139/JKSAS.2004.32.9.103

Mechanical System Design and Development of the HAUSAT-1 Picosatellite  

Hwang, Ki-Lyong (한국항공대학교 대학원)
Min, Myung-Il (한국항공대학교 대학원)
Moon, Byoung-Young (한국항공대학교 대학원)
Chang, Young-Keun (한국항공대학교 항공우주 및 기계공학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.32, no.9, 2004 , pp. 103-113 More about this Journal
Abstract
The satellite is exposed to the severe vibration environments such as random vibration environments such as random vibration, acceleration, shock, and acoustics during launch ascent and transportation. It is also faced with various space environments such as thermal vacuum, radiation and microgravity during the mission life. The satellite should be designed, manufactured, assembled and tested to be able to endure in these harsh environments. This paper addresses the results of the structural and thermal design and analyses for the HAUSAT-1 picosatellite which is scheduled to launch in the first quarter of 2005 by Russian launch vehicle "Dnepr". The qualification vibration and thermal vacuum tests have been conducted and passed at the satellite level to ensure that the HAUSAT-1 mechanical system was designed to be stable with enough margin.
Keywords
Launch Environmental Test; Thermal Vacuum Test; Qualification/Flight Model; FEA; CubeSat;
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