论文标题
在立方体平台上进行伽马射线爆发检测的紧凑型仪器II:详细的设计,组装和验证
A compact instrument for gamma-ray burst detection on a CubeSat platform II: Detailed design, assembly and validation
论文作者
论文摘要
伽马射线模块GMOD是一个小型的新型伽马射线检测器,它将是教育爱尔兰研究卫星(EIRSAT-1)2U CUCESAT任务的主要科学有效载荷。 GMOD包括一个紧凑型(25mm $ \ times $ 25mm $ \ times $ 40mm)溴化晶状体闪光灯,与4 $ \ times 4 $ \ times $ 4的瓷砖阵列相连,并带有由IDE3380 siphra提供的前端读数。本文介绍了详细的GMOD设计和仪器在限制性立方体形式中的容纳。电子和机械接口与许多现成的立方体系统和结构兼容。 GMOD工程资格模型的能量响应已使用放射性来源确定,并且已经测量了662KeV时的能量分辨率为5.4%。 EIRSAT-1将执行GMOD数据的板载处理。触发结果,包括光曲线和光谱,将被纳入航天器信标,并连续传输。便宜的硬件可用于解码信标信号,从而使数据可以访问广泛的社区。 除EIRSAT-1任务的教育和技术演示目标外,GMOD还将具有检测伽马射线爆发的科学能力。迄今为止,详细的设计和测量结果表明了GMOD在低地球轨道中的能力,较大立方体的设计可扩展性以及未来大型伽马射线任务的元素。
The Gamma-ray Module, GMOD, is a miniaturised novel gamma-ray detector which will be the primary scientific payload on the Educational Irish Research Satellite (EIRSAT-1) 2U CubeSat mission. GMOD comprises a compact (25mm $\times$ 25mm $\times$ 40mm) cerium bromide scintillator coupled to a tiled array of 4$\times$4 silicon photomultipliers, with front-end readout provided by the IDE3380 SIPHRA. This paper presents the detailed GMOD design and the accommodation of the instrument within the restrictive CubeSat form factor. The electronic and mechanical interfaces are compatible with many off-the-shelf CubeSat systems and structures. The energy response of the GMOD engineering qualification model has been determined using radioactive sources, and an energy resolution of 5.4% at 662keV has been measured. EIRSAT-1 will perform on-board processing of GMOD data. Trigger results, including light-curves and spectra, will be incorporated into the spacecraft beacon and transmitted continuously. Inexpensive hardware can be used to decode the beacon signal, making the data accessible to a wide community. GMOD will have scientific capability for the detection of gamma-ray bursts, in addition to the educational and technology demonstration goals of the EIRSAT-1 mission. The detailed design and measurements to date demonstrate the capability of GMOD in low Earth orbit, the scalability of the design for larger CubeSats and as an element of future large gamma-ray missions.