自主火星探测高集成离子与中性粒子分析仪

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doi:10.15982/j.issn.2095-7777.2019.02.005

1.
中国科学院国家空间科学中心, 北京 100190;天基空间环境探测北京市重点实验室, 北京 100190;中国科学院空间环境态势感知技术重点实验室, 北京 100190
2.
中国科学院国家空间科学中心, 北京 100190;天基空间环境探测北京市重点实验室, 北京 100190;中国科学院空间环境态势感知技术重点实验室, 北京 100190;中国科学院大学, 北京 100049
3.
中国科学院国家空间科学中心, 北京 100190;天基空间环境探测北京市重点实验室, 北京 100190;中国科学院空间环境态势感知技术重点实验室, 北京 100190;中国科学院大学, 北京 100049;空间天气国家重点实验室, 北京 100190

基金项目:自主火星探测计划资助项目（MARSY601-1-H）；中国科学院重点部署资助项目（ZDRW-KT-2019-1-01）

Integrated Ion and Neutral Particle Analyzer for Chinese Mars Mission

1.
National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China;Beijing Key Laboratory of Space Environment Exploration, Beijing 100190, China;Key Laboratory of Environmental Space Situation Awareness Technology, Beijing 100190, China
2.
National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China;Beijing Key Laboratory of Space Environment Exploration, Beijing 100190, China;Key Laboratory of Environmental Space Situation Awareness Technology, Beijing 100190, China;University of Chinese Academy of Sciences, Beijing 100049, China
3.
National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China;Beijing Key Laboratory of Space Environment Exploration, Beijing 100190, China;Key Laboratory of Environmental Space Situation Awareness Technology, Beijing 100190, China;University of Chinese Academy of Sciences, Beijing 100049, China;State Key Laboratory of Space Weather, Beijing 100190, China

摘要:小型化、高集成化是深空探测载荷发展的主要趋势。在我国自主火星探测计划中，设计了一种高集成化的火星离子与中性粒子分析仪。采用从传感器到电子学进行最大限度共用的设计思路，在一台仪器中实现对离子和能量中性原子进行能量、方向和成分的探测，大大降低了仪器对卫星平台的资源需求。仪器采取静电分析进行离子的方向和能量测量、采取飞行时间方法进行离子成分的测量。中性原子采用电离板电离成带电离子，后端的能量测量和成分测量与离子相同。鉴定件样机已经完成了初步的测试定标，结果表明其满足设计要求。
- 高集成化/
- 火星/
- 离子/
- 能量中性原子/
- 分析仪
Abstract:The miniature and integrated design is a main trend in science payload development for deep space. An integrated ion and neutral particle analyzer is built for Chinese Mars exploration project. The measurements of ion and energetic neutral atom share the sensor and electronics and are integrated in a single instrument with lower mass and power. Electrostatic analyzing method is used to measure the ions'energy and direction. Time of flight method is used to measure the ions species. The energetic neutral atoms are ionized firstly and the same measurement method with ions. The qualification model is calibrated and the results fulfill the requirements for the Mars project.
- integrated design/
- Mars/
- ion/
- energetic neutral atom/
- analyzer

[1]	SNYDER C W,NEUGEBAUER M. The mission for Mariner Ⅱ:preliminary observations,Solar plasma experiment[J]. Science,1962, 138(3454):1095-1100.
[2]	FARMER C B,DAVIES,D W,HOLLAND A L,et al. Mars:water vapour observations from THE Viking orbiters[J]. Journal of Geophysical Research,1977,82(28):4225-4248.
[3]	VERIGIN M,GRINGAUZ K I,KOTOVA G A,et al. On the problem of the martian atmosphere dissipation:PHOBOS 2 AUS spectrometer results[J]. Journal of Geophysical Research,1991,96(19):315-320.
[4]	MITCHELL D L,LIN R P,MAZELLE C,et al. Probing Mars' crustal magnetic field and ionosphere with the MGS electron reflector meter[J]. Journal of Geophysical Research,2001,106(E10):23419-23427.
[5]	BARABASH S,LUNDIN R,ANDERSSON H,et al. The analyzer of space plasmas and energetic atoms(ASPERA-3)for the Mars express mission[J]. Space Science Reviews,2006,126(1-4):113-164.
[6]	MCFADDEN J P,KORTMANN O,CURTIS D,et al. MAVEN suprathermal and thermal ion composition(STATIC)Instrument[J]. Space Science Reviews,2015,195(1-4):199-256.
[7]	LI L,WANG S J,ZHANG A B,et al. The plasma experiment of the YH-1 mission[C]//Seventh International Symposium on Instrumentation and Control Technology:Optoelectronic Technology and Instruments,Control Theory and Automation,and Space Exploration. Beijing:The International Society for Optical Engineering,2008.
[8]	孔令高,张爱兵,王世金,等. 基于SIMION软件的空间等离子体探测器的数值仿真[J]. 中国空间科学技术,2012,32(4):71-76. KONG L G,ZHANG A B,WANG S J,et al. Numeric simulation analysis of a miniature space plasma analyzer by SIMION[J]. Chinese Space Science and Technology,2012,32(4):71-76.
[9]	GRUNTMAN M. Neutral atom imaging[J]. Review of Scientific Instrument,1997,68(10):3617-3656.
[10]	FUSELIER S A,BOCHSLER P,CHORNAY D,et al. The IBEX-Lo sensor[J]. Space Science Reviews,2009,146(1-4):117-147.
[11]	MOORE T E,CHORNAY D J,COLLIER M R,et al. The lowenergy neutral atom imager for IMAGE[J]. Space Science Reviews, 2000,91(1/2):155-195.
[12]	WIESER M,WURZ P. Production of a 10~1000 eV neutral particle beam using surface neutralization[J]. Measurement Science and Technology,2005,16(12):1511-2516.
[13]	ALLEGRINI F,WIMMER-SCHWEINGRUBER R F,WURZ P,et al. Determination of low-energy ion-induced electron yields from thin carbon foils[J]. Nuclear Instruments and Methods in Physics Research,2003,211(4):487-494
[14]	WUEST M. Time-of-flight ion composition measurement technique for space plasmas[C]//Measurement Techniques in Space PlasmasParticles:Geophysical Monograph 102. Washington,DC:Geophysical Monograph Series,102,American Geophysical Union,1998:141-155.
[15]	GLOECKLER G. Ion composition measurement techniques for space plasmas[J]. Review of Science Instruments,1990,61(11):3613-3620
[16]	GALVIN A B,KISTLER L M,POPECKI M A,et al. The plasma and suprathermal ion composition(PLASTIC)investigation on the STEREO observatories[J]. Space Science Reviews,2008,136(1-4):437-486
[17]	REME H,BOSQUED J M,SAUVAUD J A,et al. The cluster ion spectrometry(CIS)experiment[J]. Space Science Reviews,1997,79(1/2):303-350
[18]	YOUG D T,BERTHELIER J J,BLANC M,et al. Cassini plasma spectrometer investigation[J]. Space Science Reviews,2004(114):1-112.
[19]	KONG L G,ZHANG A B,ZHENG X Z,et al. A satellite-boren miniature ion mass spectrometer for space plasma[J]. Chinese Journal of Space Science,2015,35(6):755-762.
[20]	孔令高,张爱兵,郑香脂,等. 热离子质谱分析仪研制及定标[J]. 空间科学学报,2017,37(5):585-592. KONG L G,ZHANG A B,ZHENG X Z,et al. Development and calibration of thermal ion mass spectrometer[J]. Chinese Journal of Space Science,2017,37(5):585-592.
[21]	WUEST M,DAVID S E,RUDOLF V S. Calibration of particle instruments in space physics[M]. Netherlands:ESA Publications Division,2007.

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自主火星探测高集成离子与中性粒子分析仪

doi:10.15982/j.issn.2095-7777.2019.02.005

Integrated Ion and Neutral Particle Analyzer for Chinese Mars Mission

计量

自主火星探测高集成离子与中性粒子分析仪

doi:10.15982/j.issn.2095-7777.2019.02.005

English Abstract

Integrated Ion and Neutral Particle Analyzer for Chinese Mars Mission

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留言板

自主火星探测高集成离子与中性粒子分析仪

doi:10.15982/j.issn.2095-7777.2019.02.005

Integrated Ion and Neutral Particle Analyzer for Chinese Mars Mission

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自主火星探测高集成离子与中性粒子分析仪

doi:10.15982/j.issn.2095-7777.2019.02.005

English Abstract

Integrated Ion and Neutral Particle Analyzer for Chinese Mars Mission

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