用于高科学回报小载荷任务的火星探测仪器

Pamela Clark, N. Barba, T. Komarek, V. Stamenković, L. Giersch, R. Woolley, C. Edwards, Robert Anderson
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引用次数: 1

摘要

喷气推进实验室的火星探测理事会正在赞助一项研究,以检查开发小型航天器任务(SSc)的技术可行性,该任务能够低成本,引人注目的科学。低成本的小型航天器任务可以在高风险类别中实现独特的任务概念,为在可能尚未探索的地区进行引人注目的科学任务创造机会,以及星座、网络、侦察和根本的新测量。适合小型航天器质量、体积、功率和成本限制的火星探测分析小组(MEPAG)高优先级调查的潜在科学仪器包括紧凑型相机(例如,火星科学实验室(MSL)增强型工程相机(EECam))、气象学(例如,MSL气象环境动力学分析仪(MEDA))、地震仪(例如,InSIGHT SEIS)、大气和微量气体(例如,MSL可调谐激光光谱仪(TLS))、尘埃(例如,ExoMars微型火星环境尘埃(MicroMED))分析仪和磁通门磁力计(InSIGHT Mag)。低成本任务概念的两个例子是LOKI(本地化有机关键成分),一个用于测量痕量气体的非静止小卫星轨道星座,以及TH2OR,一个能够探测到许多公里深度的水的时域电磁探测仪,它将通过一个小型高冲击能量装置(SHIELD)着陆。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Instrumentation for Exploring Mars with High Science Return Small Payload Missions
The Mars Exploration Directorate at the JPL is sponsoring a study to examine technical feasibility of developing small spacecraft missions (SSc) capable of low-cost, compelling science. Low cost small spacecraft missions can enable unique mission concepts in higher risk classes creating opportunities for compelling science missions in regions that may be otherwise remain unexplored, as well as for constellations, networks, scouts, and fundamentally new measurements. Potential science instruments for Mars Exploration Analysis Group (MEPAG) high-priority investigations suited to small spacecraft mass, volume, power, and cost constraints include compact versions of a camera (e.g., Mars Science Laboratory (MSL) Enhanced Engineering Camera (EECam)), Meteorology (e.g., MSL Meteorology Environmental Dynamics Analyzer (MEDA)), Seismometer (e.g., InSIGHT SEIS), Atmosphere and Trace Gases (e.g., MSL Tunable Laser Spectrometer (TLS)), Dust (e.g., ExoMars Micro Mars Environmental Dust (MicroMED)) analyzers, and fluxgate magnetometers (InSIGHT Mag). Two examples of low-cost mission concepts are LOKI (Localizing Organic Key Ingredients), an areostationary SmallSat orbital constellation designed to measure trace gases, and TH2OR, a time-domain EM sounder capable of water detection to a depth of many kilometers, which would be landed via a small high impact energy device (SHIELD).
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