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IN-FLIGHT PERFORMANCE OF THE VAN ALLEN PROBES RF TELECOMMUNICATIONS SYSTEM

机译:范·艾伦探针无线通信系统的机上性能

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The NASA Van Allen Probes mission (previously called the Radiation Belt Storm Probes) successfully launched on 30 August, 2012. The twin spacecraft, designed, built, and operated by The Johns Hopkins University Applied Physics Laboratory (JHU/APL), have been successfully operating within Earth's radiation belts since then, returning critical science data revealing new insights into the physics of the radiation belts. Because of the extreme radiation environment, all spacecraft subsystems including the telecommunications system had to make special accommodations to withstand the effects of the radiation. Each Van Allen Probes spacecraft's telecommunications systems includes an S-band version of the Frontier Radio, a solid-state power amplifier, RF routing components, and dual low-gain antennas. This mission marks the first flight of the Frontier Radio, which is baselined for use in the upcoming Solar Probe Plus and Europa Clipper missions. This paper will present an overview of the as-built telecommunications system and its ground station interfaces, discuss key communications flight hardware components, and then discuss in detail activities and performance in-flight, including launch and commissioning operations, performance enhancements since launch, and performance trending in flight. Post-launch telecommunications commissioning activities were driven by the requirement to verify both spacecraft's communication systems over multiple ground networks, including JHU/APL's own 18-m ground station, the Universal Space Network, and TDRSS. Enhanced science data downlink volume was enabled by expanding the iusable field of view of the spacecrafts' antennas once in-flight, calibrations of the antenna patterns were completed, as well as reducing downlink link margins to a bare minimum when downlinking via APL's 18-m dish, where the CFDP (CCSDS File Delivery Protocol) is used to guarantee file delivery. Radiation drove some of the hardware design;the radios have experienced several predicted fault conditions at the predicted rates, and have reacted autonomously as designed to minimize impact to the science downlink. The communications system was originally designed to meet a 2-ycar minimum science campaign. Assuming the system and the rest of the spacecraft continue to operate as expected, this mission may be extended to enable the return of further science from the relatively ill-explored Van Allen Radiation Belts.
机译:2012年8月30日,NASA范艾伦探测器任务(以前称为辐射带风暴探测器)成功发射。由约翰·霍普金斯大学应用物理实验室(JHU / APL)设计,建造和运营的双星飞船已经成功完成此后,它在地球的辐射带内运行,返回的关键科学数据揭示了对辐射带物理的新见解。由于极端的辐射环境,所有航天器子系统(包括电信系统)都必须进行特殊调整以承受辐射的影响。每个Van Allen Probes航天器的电信系统都包括Frontier Radio的S波段版本,固态功率放大器,RF路由组件和双低增益天线。该任务标志着Frontier Radio的首次飞行,该基线被基线用于即将到来的Solar Probe Plus和Europa Clipper任务。本文将概述已建成的电信系统及其地面站接口,讨论关键的通信飞行硬件组件,然后详细讨论飞行中的活动和性能,包括发射和调试操作,自发射以来的性能增强以及飞行中的性能趋势。发射后的电信调试活动是由验证两个航天器通过多个地面网络(包括JHU / APL自己的18米地面站,通用空间网络和TDRSS)的通信系统的需求驱动的。通过在飞行中扩大航天器天线的可视范围,完成天线方向图的校准以及在通过APL的18-m下行链路将下行链路链路余量降低到最小时,可以增强科学数据的下行链路容量盘,其中CFDP(CCSDS文件传送协议)用于保证文件传送。辐射推动了某些硬件设计;无线电设备已经以预测的速率经历了几个预测的故障情况,并且按照设计的要求进行了自主反应,以最大程度地减少对科学下行链路的影响。该通信系统最初是为满足2轮汽车最低限度的科学运动而设计的。假设系统和航天器的其余部分继续按预期运行,则该任务可能会延长,以使人们能够从相对欠发达的范艾伦辐射带上获得更多的科学成果。

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