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The high reliability southwest LEO Explorer (SLX-6) CubeSat bus

机译:高可靠性西南LEO Explorer(SLX-6)CubeSat总线

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Southwest Research Institute (SwRI) has developed the Southwest LEO EXplorer (SLX-6), a standard 6U CubeSat in a 2U ¿¿ 3U form factor intended to carry a payload into a variety of Low Earth Orbits. SLX-6 also serves as the basis for the Southwest Deep-Space Explorer (SDX-6) that SwRI is developing for the CubeSat mission to study Solar Particles (CuSP) mission (Figure 2). The SLX-6 is built to a tailored NPR-7120 approach adapted from SwRI's experience in Class B, C, and D missions. Program execution will include bus component selection, testing, and analysis; mechanical design and analysis (structural and thermal); bus and Attitude Determination and Control Subsystem (ADCS) flight software (FSW) definition and tailoring; bus Electrical Ground Support Equipment (which transitions into the ground data system); Assembly Integration and Testing (AI&T) including Thermal Vacuum (TVAC), Vibration (Vibe), Shock (as needed), and EMI/EMC environmental testing; and NASA operations support. The SLX-6 is novel in three distinct ways when compared to other off-the-shelf CubeSat solutions: the SLX-6 is a high reliability bus; it is robust to all space environments, including radiation; and SwRI offers a one-stop-shop for all portions of a satellite mission. The SLX-6 is designed with a robust parts program that is derived and tailored from EEE-INST-002 to be cost competitive. This same parts program is invoked when selecting radiation tolerant components. Analysis is performed in-house to ensure that the mechanical design of the observatory is compatible with environments in GEVS (GSFC-STDF-7000A). SwRI has extensive experience with all portions of satellite design and test: electrical analysis, design, and test; mechanical analysis, design, and test; flight software analysis, design, and test; component- and bus-level integration, testing, and qualification. SwRI is also presently evaluating quotes a 13meter multi-band ground station on campus. This paper will address the CubeS- t description, subsystems, analysis and testing philosophies, and integration and testing approach.
机译:西南研究所(SwRI)开发了西南LEO EXplorer(SLX-6),这是一种标准的6U立方体卫星,采用2U-3U尺寸,旨在将有效载荷携带到各种低地球轨道中。 SLRI-6也是SwRI为CubeSat任务开发的西南深太空探索器(SDX-6)的基础,该任务用于研究太阳粒子(CuSP)任务(图2)。 SLX-6是根据NPR-7120量身定制的方法而构建的,该方法是根据SwRI在B,C和D类任务中的经验而改编的。程序执行将包括总线组件的选择,测试和分析;机械设计和分析(结构和热学);公共汽车和姿态确定与控制子系统(ADCS)飞行软件(FSW)的定义和定制;总线电气地面支持设备(过渡到地面数据系统);组装集成和测试(AI&T),包括热真空(TVAC),振动(Vibe),冲击(根据需要)和EMI / EMC环境测试;以及NASA的运营支持。与其他现成的CubeSat解决方案相比,SLX-6在三种不同的方面具有新颖性:SLX-6是高可靠性总线;它对包括辐射在内的所有空间环境都十分坚固; SwRI为卫星任务的所有部分提供一站式服务。 SLX-6设计有强大的零件程序,该程序是从EEE-INST-002衍生和定制的,以具有成本竞争力。选择耐辐射组件时,将调用相同的零件程序。内部进行分析以确保天文台的机械设计与GEVS(GSFC-STDF-7000A)中的环境兼容。 SwRI在卫星设计和测试的各个方面均具有丰富的经验:电气分析,设计和测试;机械分析,设计和测试;飞行软件分析,设计和测试;组件级和总线级的集成,测试和鉴定。 SwRI还在评估校园中一个13米多频段地面站的报价。本文将讨论多维数据集描述,子系统,分析和测试理念以及集成和测试方法。

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