日本地球惑星科学連合2015年大会

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インターナショナルセッション(ポスター発表)

セッション記号 P (宇宙惑星科学) » P-PS 惑星科学

[P-PS04] International Collaboration in Planetary and Space Sciences: Small Projects, Big Missions, Everything

2015年5月27日(水) 18:15 〜 19:30 コンベンションホール (2F)

コンビーナ:*佐々木 晶(大阪大学大学院理学研究科宇宙地球科学専攻)、吉川 顕正(九州大学大学院理学研究院地球惑星科学部門)、Steven Vance(Jet Propulsion Laboratory, Caltech)、Kunio Sayanagi(ハンプトン大学)、関根 康人(東京大学大学院新領域創成科学研究科複雑理工学専攻)、橘 省吾(北海道大学大学院理学研究院自然史科学専攻地球惑星システム科学分野)

18:15 〜 19:30

[PPS04-P05] THE ATMOSPHERIC CHARACTERIZATION FOR EXPLORATION AND SCIENCE (ACES) INSTRUMENT SUITE FOR MARS.

*Scot RAFKIN1Don BANFIELD2John ANDREWS1Keith NOWICKI1Traci CASE1Richard DISSLY3Alicia DWYER-CIANCIOLO4Lori FENTON5Maria GENZER6Ozgur KARATEKIN7Carlos LANGE8John MERRISON9Kerry NEAL1 (1.Southwest Research Institute、2.Cornell University、3.Ball Aerospace and Technology Corp.、4.NASA Langley Research Center、5.SETI、6.Finnish Meteorological Institute、7.Royal Belgian Observatory、8.University of Alberta、9.University of Aarhus)

キーワード:Mars, Meteorology, Atmosphere, Instrumentation, Mars Mission

The Atmospheric Characterization for Exploration and Science (ACES) instrument suite is designed to address the highest priority, lower atmosphere goals and investigations identified by MEPAG[1] and to address both exploration technology Strategic Knowledge Gaps (SKGs)[2]. The ACES instrument suite measures atmospheric dust properties, fundamental atmospheric parameters, and the energy inputs that drive the atmosphere in ways that far exceed previous landed experiments.

The data to be returned by ACES is the compre-hensive and necessary type of information that has been sought after by the atmospheric, aeolian, and Entry, Descent, and Landing (EDL) communities since the Viking Landers provided the first in situ glimpse of Martian meteorology. The intervening experiments since Viking have only marginally increased the knowledge necessary to address Mars Exploration Program and Human Exploration and Operations Mission Directorate (HEOMD) goals; continuing to repeat these meteorological experiments is an exercise in diminishing returns.

In addition to temperature, pressure, and relative humidity, ACES measures for the first time airborne particle concentration and size distribution, 3D wind components, and infrared and visible radiative fluxes. By combining the unique capabilities of ACES to de-termine turbulent eddy momentum fluxes and dust characteristics, ACES also measures the wind stress that lifts sand and dust.
The ACES instrument sensors may be accomodat-ed on a rover (Figure 1) or an a stationary lander. A boom for wind and temperature and in some cases vis and IR radiation flux minimizes potential thermal, mechanical and radiative contamination by the space-craft.

ACES is strengthened by internationally contribut-ed sensors and electronics from the U.S.A., Finland, Denmark, Canada, and Belgium. The ACES science team is comprised of exceptional scientists and engi-neers from each of these countries.
Details on the capabilities and response of each in-strument, power requirements, accommodation, ob-servation strategy, and data products and volume will be detailed in the talk.

References
[1] MEPAG (2008), Mars Scientific Goals, Objectives, Investigations, and Priorities: 2008, J.R. Johnson, ed. [2] Precursor Strategy Analysis Group (P-SAG) (2012) Report.