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The design and implementation of a high sensitivity telescope for in situ measurements of energetic particles in the Earth's radiation belts.

机译:用于现场测量地球辐射带中高能粒子的高灵敏度望远镜的设计和实现。

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摘要

This work describes the design and implementation of a high-sensitivity telescope (HST) for in situ detection and energy analysis of energetic charged particles in the Earth's radiation belts from a near-equatorial orbit that will range over geocentric distances from ≈ 2--3.5 Earth radii as part of the US Air Force's Demonstrations and Science eXperiment (DSX) mission. The HST employs a two element silicon solid state detector telescope that has a geometrical factor of 0.1 cm2 sr with a 14° field-of-view centered on the on-orbit local magnetic field vector to detect ≈ 100 particles s-1 cm-2 sr-1 in the geomagnetic bounce loss cone. The pointing direction of the HST is guaranteed by the active attitude control subsystem of the spacecraft. A novel implementation of a knife-edged baffled collimator design restricts the field-of-view and provides a sharp cutoff (≈ 103) in the angular response to all particle species with energies from ≈ 40--800 keV. The HST detectors are shielded with 5g cm-2 of aluminum followed by 3.1 g cm-2 of tungsten in all non-look directions to reduce the background fluxes incident on the detectors through the orbit (>107 particles cm -2 s-1 for electrons and protons individually) to levels that will allow the detection of the target flux in the loss cone.;The HST has been extensively characterized on the ground and is capable of analyzing the energies of particles over the range of 25--850 keV with an energy resolution of 3.7keV and a noise FWHM of 15keV. The calibration has been established using 241Am and 133Ba X-ray sources and verified using additional beta- and X-ray sources and the electron beams produced by the 2 MeV Van de Graaff accelerator at the NASA Goddard Spaceflight Center's Radiation Effects Facility. The instrument's calibration has been shown to vary by less than 2% over the operational temperature range of --20 to +35°C. Electromagnetic interference testing has proven that the HST is unaffected by strong VLF fields of peak amplitude 1.5 kV.
机译:这项工作描述了高灵敏度望远镜(HST)的设计和实现,该望远镜用于从近赤道轨道对地球辐射带中的高能带电粒子进行原位检测和能量分析,该范围将在距≈地心距的范围内。 2--3.5地球半径,是美国空军的示范和科学实验(DSX)任务的一部分。 HST使用两元素硅固态探测器望远镜,其几何因子为0.1 cm2 sr,以在轨局部磁场矢量为中心的14°视场可以探测和探测卫星。地磁反弹损耗锥中的100个粒子s-1 cm-2 sr-1。 HST的指向方向由航天器的主动姿态控制子系统来保证。带有刀口的挡板式准直器设计的新颖实现方式限制了视场,并利用来自≈的能量提供了对所有粒子种类的角度响应的清晰截止(≈ 103)。 40--800 keV。 HST探测器用5 g cm-2的铝屏蔽,然后用3.1 g cm-2的钨在所有非可视方向上屏蔽,以减少通过轨道入射在探测器上的背景通量(> 107粒子cm -2 s-1电子和质子分别)到可以检测损耗锥中目标通量的水平; HST已在地面上进行了广泛表征,并能够分析25--850 keV范围内的粒子能量能量分辨率为3.7keV,噪声FWHM为15keV。已使用241Am和133Ba X射线源建立了校准,并使用了额外的β和X射线源以及NASA Goddard航天中心辐射效应设施的2 MeV Van de Graaff加速器产生的电子束进行了验证。已证明仪器的校准在--20至+ 35°C的工作温度范围内变化小于2%。电磁干扰测试已证明,HST不受峰值幅度为1.5 kV的强VLF场的影响。

著录项

  • 作者

    Parker, Charles Walter.;

  • 作者单位

    Boston University.;

  • 授予单位 Boston University.;
  • 学科 Engineering Electronics and Electrical.;Physics Elementary Particles and High Energy.;Physics Astronomy and Astrophysics.
  • 学位 Ph.D.
  • 年度 2011
  • 页码 435 p.
  • 总页数 435
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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