首页> 外文期刊>Space Science Reviews >Combined Instrumentation Package COMARS+ for the ExoMars Schiaparelli Lander
【24h】

Combined Instrumentation Package COMARS+ for the ExoMars Schiaparelli Lander

机译:组合仪器套装+ Exomars Schiaparelli着陆器

获取原文
获取原文并翻译 | 示例
           

摘要

In order to measure aerothermal parameters on the back cover of the ExoMars Schiaparelli lander the instrumentation package COMARS+ was developed by DLR. Consisting of three combined aerothermal sensors, one broadband radiometer sensor and an electronic box the payload provides important data for future missions. The aerothermal sensors called COMARS combine four discrete sensors measuring static pressure, total heat flux, temperature and radiative heat flux at two specific spectral bands. The infrared radiation in a broadband spectral range is measured by the separate broadband radiometer sensor. The electronic box of the payload is used for amplification, conditioning and multiplexing of the sensor signals. The design of the payload was mainly carried out using numerical tools including structural analyses, to simulate the main mechanical loads which occur during launch and stage separation, and thermal analyses to simulate the temperature environment during cruise phase and Mars entry. To validate the design an extensive qualification test campaign was conducted on a set of qualification models. The tests included vibration and shock tests to simulate launch loads and stage separation shocks. Thermal tests under vacuum condition were performed to simulate the thermal environment of the capsule during the different flight phases. Furthermore electromagnetic compatibility tests were conducted to check that the payload is compatible with the electromagnetic environment of the capsule and does not emit electromagnetic energy that could cause electromagnetic interference in other devices. For the sensor heads located on the ExoMars back cover radiation tests were carried out to verify their radiation hardness. Finally the bioburden reduction process was demonstrated on the qualification hardware to show the compliance with the planetary protection requirements. To test the actual heat flux, pressure and infrared radiation measurement under representative conditions, a
机译:为了测量exomarsSchiaparelli着陆器的后盖上的空气热量参数,仪表包彗星+是由DLR开发的。由三个组合的空气传感器组成,一个宽带辐射计传感器和电子盒的有效载荷为未来任务提供了重要数据。称为彗星的空气感传感器结合了四个离散的传感器,测量两个特定光谱带的静压,总热量,温度和辐射热通量。宽带光谱范围内的红外辐射由单独的宽带辐射计传感器测量。有效载荷的电子盒用于传感器信号的放大,调节和复用。有效载荷的设计主要是使用包括结构分析的数控工具进行,以模拟发射和阶段分离期间发生的主机械载荷,以及在巡航相和火星入口期间模拟温度环境的热分析。为了验证设计,在一组资格模型上进行了广泛的资格测试活动。测试包括振动和冲击测试以模拟发射负载和阶段分离冲击。进行真空条件下的热试验以在不同的飞行阶段模拟胶囊的热环境。此外,进行电磁兼容性测试以检查有效载荷与胶囊的电磁环境兼容,并且不会发出可能导致其他设备电磁干扰的电磁能量。对于位于外辐射的传感器头部,进行辐射测试以验证其辐射硬度。最后,在资格硬件上证明了生物上的减少过程,以符合行星保护要求的遵守情况。在代表性条件下测试实际的热通量,压力和红外辐射测量,a

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号