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Germanium gamma-ray spectrometer PGS for the MARS-96 mission

机译:Mars-96任务的锗伽马射频光谱仪PGS

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The precision gamma-ray spectrometer (PGS) on the Russian MARS-96 spacecraft is designed to measure 0.1-8 MeV gamma rays in order to determine the elemental composition of the Martian surface, to study solar flares, and to determine energy spectra and times of arrival of gamma-ray bursts. The PGS instrument contains two high-purity, n-type germanium crystals, each similar to the one used on the Mars observer mission. Each crystal is contained in a titanium can with helicoflex cryogenic metal seals. An annealing capability allows repair of radiation damage. The detectors are cooled via nitrogen heat pipes attached to a passive radiator mounted on the back side of a solar panel. The radiators are designed to keep the Ge detectors below 100 K during the interplanetary flight. The electronics include first-stage electronics mounted on each crystal can and 4096-channel pulse height analyzers. Two parallel channels of electronics are provided and can be cross-switched by telecommands. In November 1995 integration of the flight detectors with flight electronics and testing of the complete system cooled by the passive radiator were successfully completed. The energy resolution degrades to about 3 keV in the flight configuration. Warming the radiators indicated that for the worst case when the radiator views Mars at the equator the maximum temperature of the detectors will be limited by the diode action of the heat pipes to 118 K. Extensive calibrations with radioactive sources are in progress. We conclude that we have an improved design for planetary and gamma-ray burst studies and the PGS instrument is ready for launch in November 1996.
机译:俄罗斯MARS-96航天器上的精密伽马射线光谱仪(PGS)旨在测量0.1-8 Mev Gamma射线,以确定Martian表面的元素组成,研究太阳能耀斑,并确定能量谱和时间伽马射线爆发的到来。 PGS仪器含有两种高纯度,N型锗晶体,每个锗晶体相似于马斯观察员任务中使用的一种。每个晶体包含在钛罐中,螺旋光源密封件。退火能力允许修复辐射损伤。探测器通过附接到安装在太阳能电池板的后侧的无源辐射器上的氮气热管冷却。散热器旨在将GE探测器保存在行星际航班期间100 k以下。电子产品包括安装在每个晶体上的一级电子设备和4096频道脉冲高度分析仪。提供了两个并行电子设备通道,可以由电信交换。 1995年11月,用飞行电子设备的飞行探测器的整合成功完成了被动散热器冷却的完整系统的测试。在飞行配置中,能量分辨率降低至约3keV。散热器表示,对于最坏的情况,对于armet的辐射器观看火星的最坏情况,检测器的最大温度将受到热管的二极管动作的限制为118k.具有放射源的广泛校准正在进行中。我们得出结论,我们对行星和伽马射线爆发的设计有所改善,PGS仪器在1996年11月开始推出。

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