12   Artículos

 
en línea
Jae-Hyeon Park, Sung-Woo Park, Jong-Pil Kim and Hyun-Ung Oh    
A novel passive vibration-damping device is proposed and investigated for a large deployable solar array. One strategy for achieving high damping in a solar panel is using a yoke structure comprising a hyperelastic shape memory alloy and multiple viscous... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shuang Wu, Zhijun Zhao, Dongping Liang, Qunzhi Li and Shougen Zhao    
Multiple linear and nonlinear dynamic parameters of the joints at the root of solar panels and between solar panels on spacecraft, both of which have complex nonlinear dynamic properties, were identified by using the force state mapping method for modeli... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shankar Bhattarai, Ji-Seong Go and Hyun-Ung Oh    
In this study, we present the Diverse Holding and Release Mechanism Can Satellite (DHRM CanSat) platform developed by the Space Technology Synthesis Laboratory (STSL) at Chosun University, South Korea. This platform focuses on several types of holding an... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shankar Bhattarai, Ji-Seong Go, Hongrae Kim and Hyun-Ung Oh    
The structural safety of solar cells mounted on deployable solar panels in the launch vibration environment is a significant aspect of a successful CubeSat mission. This paper presents a novel highly damped deployable solar panel module that is effective... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Amber E. Keith, Jesse J. French     Pág. 30 - 36
The design of an all-inclusive, self-sufficient, sustainable water purification system for application in developing regions of the world can improve living conditions for people world-wide, especially in regions where access to clean drinking water is l... ver más
Revista: Advances in Technology Innovation    Formato: Electrónico

 
en línea
Syahrim Azhan Ibrahim and Eiki Yamaguchi    
Nanosatellites, like CubeSat, have begun completing advanced missions that require high power that can be obtained using deployable solar panels. However, a larger solar array area facing the Sun increases the solar radiation torque on the satellite. In ... ver más
Revista: Aerospace    Formato: Electrónico

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