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The protoMIRAX hard X-ray imaging balloon experiment

机译:protoMIRAX硬X射线成像气球实验

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Context. The protoMIRAX hard X-ray imaging telescope is a balloon-borne experiment developed as a pathfinder for the MIRAX satellite mission. The experiment consists essentially in a coded-aperture hard X-ray (30–200 keV) imager with a square array (13 × 13) of 2 mm-thick planar CZT detectors with a total area of 169 cm2. The total, fully-coded field-of-view is 21° × 21° and the angular resolution is 1°43′. Aims. The main objective of protoMIRAX is to carry out imaging spectroscopy of selected bright sources to demonstrate the performance of a prototype of the MIRAX hard X-ray imager. In this paper we describe the protoMIRAX instrument and all the subsystems of its balloon gondola, and we show simulated results of the instrument performance. Methods. Detailed background and imaging simulations were performed for protoMIRAX balloon flights. The 3σ sensitivity for the 30–200 keV range is ~1.9 × 10-5 photons?cm-2?s-1 for an integration time of 8 h at an atmospheric depth of 2.7 g?cm-2 and an average zenith angle of 30°. We developed an attitude-control system for the balloon gondola and new data handling and ground systems that also include prototypes for the MIRAX satellite. Results. We present the results of Monte Carlo simulations of the camera response at balloon altitudes, showing the expected background level and the detailed sensitivity of protoMIRAX. We also present the results of imaging simulations of the Crab region. Conclusions. The results show that protoMIRAX is capable of making spectral and imaging observations of bright hard X-ray source fields. Furthermore, the balloon observations will carry out very important tests and demonstrations of MIRAX hardware and software in a near space environment.
机译:上下文。 protoMIRAX硬X射线成像望远镜是气球飞行实验,是为MIRAX卫星任务探路而开发的。该实验主要包括一个编码孔径硬X射线(30–200 keV)成像器,该成像器具有2毫米厚的平面CZT检测器的正方形阵列(13×13),总面积为169 cm2。完全编码的总视场为21°×21°,角分辨率为1°43'。目的protoMIRAX的主要目的是对选定的亮光源进行成像光谱分析,以证明MIRAX硬X射线成像仪原型的性能。在本文中,我们描述了protoMIRAX仪器及其球囊吊舱的所有子系统,并显示了仪器性能的模拟结果。方法。对protoMIRAX气球飞行进行了详细的背景和成像模拟。在大气深度为2.7 g?cm-2和平均天顶角为8 h的情况下,对于8 h的积分时间,在30–200 keV范围内的3σ灵敏度为〜1.9×10-5光子?cm-2?s-1。 30°。我们开发了用于气球吊舱的姿态控制系统以及新的数据处理和地面系统,其中还包括MIRAX卫星的原型。结果。我们介绍了在气球高度相机响应的蒙特卡罗模拟结果,显示了预期的背景水平和protoMIRAX的详细灵敏度。我们还介绍了蟹区域的成像模拟结果。结论。结果表明protoMIRAX能够对明亮的硬X射线源场进行光谱和成像观察。此外,气球观测将在近太空环境中对MIRAX硬件和软件进行非常重要的测试和演示。

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