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SPACE EXPLORATION SYMPOSIUM (A3) Mars Exploration - Science, Instruments and Technologies (3B) EXOMARS ENTRY, DESCENT AND LANDING SCIENCE

机译:太空勘探研讨会(A3)火星勘探 - 科学,仪器和技术(3B)屈光度入境,下降和着陆科学

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The Entry, Descent and Landing System (EDLS) of an atmospheric entry probe or lander requires measurements in order to trigger the events of the descent sequence. These measurements besides being aimed to guarantee a safe landing, could provide essential information for the study of planetary atmosphere. Few in situ probes have entered the atmosphere of planetary bodies such as Mars, Venus, Jupiter and Titan, the largest moon of Saturn. EDL phases are critical with reference to mission achievement and require development and validation of technologies linked to the environmental and aerodynamical conditions the vehicle will face. An accurate knowledge of the dynamics of the probe during entry and descent (i.e. trajectory and attitude determination) allows the retrieval of the atmospheric vertical profile of values such as density, temperature and pressure at a vertical resolution far higher than previously explored and/or reachable by remote sensing. The entry, descent and landing of the ExoMars program offer a rare (once-per-mission) opportunity to perform in situ investigations of the martian environment over a wide altitude range. ExoMars 2016 Descent Module and 2018 Surface Platform will provide new direct in situ measurements at different sites, season and time period complementing the few atmospheric profiles derived by previous probes (e.g. Viking 1 & 2, Mars PathFinder, Mars Exploration Rovers and Phoenix). The ExoMars AMELIA (Atmospheric Mars Entry and Landing Investigations and Analysis) team seeks to exploit the EDLS engineering measurements for scientific investigations of Mars' atmosphere and surface. From the measurements recorded during entry and descent, using similar methods and analysis employed on previous entry probe missions (e.g. ESA Huygens at Titan, NASA Mars PathFinder, MERs, Phoenix, MSL-Curiosity) we will retrieve an atmospheric vertical profile along the entry and descent trajectory. These data will contribute to exploring an altitude range not covered by an orbiter, providing surface and atmosphere "ground truths" for remote sensing observations and important constrains for updates and validations of the Mars atmosphere General Circulation models. We will present our proposed methodology and objectives for exploiting the ExoMars EDLS measurements beyond their expected engineering information for scientific investigations of Mars' environment.
机译:大气进入探针或着陆器的入口,下降和着陆系统(EDL)需要测量以触发下降序列的事件。这些测量除了旨在保证安全着陆,可以为行星气氛的研究提供必要的信息。少数人探讨已经进入了行星体的气氛,如火星,金星,木星和泰坦,土星最大的月亮。 EDL阶段对任务成就至关重要,需要开发和验证与车辆将面临的环境和空气动力学条件相关的技术。准确地了解进入和下降期间探针的动态(即轨迹和姿态确定)允许检索诸如密度,温度和压力的值的大气垂直轮廓,其垂直分辨率远远高于先前探索和/或可达的垂直分辨率通过遥感。 ExoMars计划的入境,下降和降落提供了罕见(每次任务)的机会,以在宽阔的高度范围内对火星环境进行现场调查。 Exomars 2016年下降模块和2018年表面平台将在不同的网站,季节和时间段提供新的直接测量,季节和时间段补充以前探测器的几种大气配置文件(例如,Viking 1和2,Mars Pathfinder,Mars Exploration Rovers和Phoenix)。 Exomars Amelia(大气火星进入和登陆和分析)队旨在利用EDLS工程测量来进行火星气氛和表面的科学调查。从进入和下降期间记录的测量,使用先前进入探针任务的类似方法和分析(例如泰坦的ESA Huygens,美国宇航局火星探路者,MERS,Phoenix,MSL Cutiosity)我们将沿进入的大气垂直型材检索下降轨迹。这些数据将有助于探索轨道器未涵盖的高度范围,为遥感观察提供表面和大气“地面真理”,以及MARS气氛通用循环模型的更新和验证的重要约束。我们将展示我们提出的方法和目标,用于利用其超出其预期工程信息的exoMars EDLS测量,以获得MARS环境的科学调查。

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