TURKSAT-3USAT: A 3U communication CubeSat with passive magnetic stabilization

A. Aslan, A. Sofyali, E. Umit, C. Tola, I. Oz, S. Gulgonul
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引用次数: 8

Abstract

TURKSAT-3USAT is a three unit CubeSat developed for voice communication at low earth orbit. The payload is a VHF/UHF transponder operating at amateur bands. The transponder and all other subsystems, except the stabilization, are doubled for redundancy. Where possible, both COTS systems and in-house development is employed. The energy is provided using lithium polymer batteries together with super capacitors. Satellite stabilization is accomplished using passive magnetic attitude control system with hysteresis rods. Based on the recent United Nations regulations and CubeSat standard, the satellite is to include a de-orbiting system which will make it reenter the atmosphere following completion of its life time. The 3USAT is foreseen to be ready for launch, early 2012.
TURKSAT-3USAT:具有无源磁稳定的3U通信立方体卫星
TURKSAT-3USAT是一种用于低地球轨道语音通信的三单元立方体卫星。有效载荷是在业余波段操作的VHF/UHF应答器。转发器和所有其他子系统,除了稳定,是双倍的冗余。在可能的情况下,同时采用COTS系统和内部开发。能量是由锂聚合物电池和超级电容器一起提供的。采用带磁滞杆的被动磁姿态控制系统实现卫星稳定。根据最近的联合国条例和立方体卫星标准,这颗卫星将包括一个离轨系统,使其在寿命结束后重新进入大气层。3USAT预计将于2012年初发射。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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