首页> 外文会议>Russian-German conference on electric propulsions and their application >Verifying parameters of ground data processing for the thermal control system of small spacecraft AIST based on telemetry data obtained by Samara University's GCS
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Verifying parameters of ground data processing for the thermal control system of small spacecraft AIST based on telemetry data obtained by Samara University's GCS

机译:基于Samara University的GCS获得的遥测数据,验证小型航天器AIST热控制系统的地面数据处理参数

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The paper presents the results of verification of ground testing of the AIST-type small spacecraft thermal control system (TCS) based on telemetry data received during their in-orbit testing and operation by the ground control station (GCS) of Samara University. The study into the efficiency and operability of the TCS was carried out on AIST series small spacecrafts AIST#1 (RS-43as), launched on April 19, 2013 from Baykonur Cosmodrome as a by-cargo of Bion-M #1 spacecraft, and an experimental sample of AIST #2 (RS-41at) small spacecraft launched by Soyuz-2.lv with the Volga insertion module on December 28, 2013, from the Plesetsk Cosmodrome.
机译:本文介绍了基于在撒玛拉大学地面控制站(GCS)的轨道测试和操作期间收到的遥测数据的遥测数据验证了辅助型小航天器热控制系统(TCS)的地面测试结果。研究了TCS的效率和可操作性的研究是在AICT系列小型航天器AIST#1(RS-43AS)上,于2013年4月19日从Baykonur Cosmodrome作为Bion-M#1 SpaceCraft的逐个货物,以及由Soyuz-2.LV推出的艾克斯#2(RS-41AT)小型航天器的实验样本,2013年12月28日,来自Plesetk Cosmodrome的Volga插入模块。

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