...
首页> 外文期刊>Geoscientific Instrumentation, Methods and Data Systems Discussions >Mars submillimeter sensor on microsatellite: sensor feasibility study
【24h】

Mars submillimeter sensor on microsatellite: sensor feasibility study

机译:MARS Sublimeter传感器在微卫星上:传感器可行性研究

获取原文
           

摘要

We present a feasibility study for a submillimeter instrument on a small Mars platform now under construction. The sensor will measure the emission from atmospheric molecular oxygen, water, ozone, and hydrogen peroxide in order to retrieve their volume mixing ratios and the changes therein over time. In addition to these, the instrument will be able to limit the crustal magnetic field, and retrieve temperature and wind speed with various degrees of precision and resolution. The expected measurement precision before spatial and temporal averaging is 15 to 25?ppmv for the molecular oxygen mixing ratio, 0.2?ppmv for the gaseous water mixing ratio, 2?ppbv for the hydrogen peroxide mixing ratio, 2?ppbv for the ozone mixing ratio, 1.5 to 2.5? μ T for the magnetic field strength, 1.5 to 2.5?K for the temperature profile, and 20 to 25?m?s ?1 ?for the horizontal wind speed.
机译:我们现在正在建设中对小火星平台上的杂交仪器仪器的可行性研究。 传感器将测量大气分子氧,水,臭氧和过氧化氢的发射,以便在其体积混合比率和随时间的时间内取回其中的变化。 除此之外,该仪器还能够利用各种精度和分辨率来限制地壳磁场,并检索温度和风速。 用于分子氧混合比的空间和时间平均前的预期测量精度为15至25〜25μpmV,为气态水混合比为0.2〜ppmv,过氧化氢混合比为2〜ppbv,臭氧混合比为2〜ppbv ,1.5到2.5? μT对于磁场强度,温度曲线为1.5至2.5?k,20至25Ω·m≤1Ω·Δ1?用于水平风速。

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