Fast Plasma Investigation for Magnetospheric Multiscale

被引：1171

作者：

Pollock, C. ^{[1
]}

Moore, T. ^{[1
]}

Jacques, A. ^{[1
]}

Burch, J. ^{[2
]}

Gliese, U. ^{[1
,3
]}

Saito, Y. ^{[4
,29
]}

Omoto, T. ^{[5
]}

Avanov, L. ^{[1
,6
]}

Barrie, A. ^{[1
,7
]}

Coffey, V. ^{[8
]}

Dorelli, J. ^{[1
]}

Gershman, D. ^{[1
,6
,9
]}

Giles, B. ^{[1
]}

Rosnack, T. ^{[1
,10
]}

Salo, C. ^{[1
,11
]}

Yokota, S. ^{[4
]}

Adrian, M. ^{[1
]}

Aoustin, C. ^{[12
]}

Auletti, C. ^{[1
,13
,14
]}

Aung, S. ^{[1
,10
]}

Bigio, V. ^{[1
]}

Cao, N. ^{[1
,15
]}

Chandler, M. ^{[8
]}

Chornay, D. ^{[1
,6
]}

Christian, K. ^{[1
,16
]}

Clark, G. ^{[1
,17
,18
]}

Collinson, G. ^{[1
,17
]}

Corris, T. ^{[1
,3
]}

De Los Santos, A. ^{[2
]}

Devlin, R. ^{[1
,3
]}

Diaz, T. ^{[2
]}

Dickerson, T. ^{[1
,19
]}

Dickson, C. ^{[1
,13
]}

Diekmann, A. ^{[8
,20
]}

Diggs, F. ^{[1
,13
]}

Duncan, C. ^{[1
]}

Figueroa-Vinas, A. ^{[1
]}

Firman, C. ^{[1
,21
]}

Freeman, M. ^{[2
]}

Galassi, N. ^{[1
,3
]}

Garcia, K. ^{[1
]}

Goodhart, G. ^{[2
]}

Guererro, D. ^{[2
]}

Hageman, J. ^{[1
]}

Hanley, J. ^{[2
]}

Hemminger, E. ^{[1
,22
]}

Holland, M. ^{[1
]}

Hutchins, M. ^{[2
]}

James, T. ^{[1
]}

Jones, W. ^{[1
,23
]}

机构：

[1] NASA, Goddard Space Flight Ctr, Greenbelt, MD USA

[2] SW Res Inst, San Antonio, TX USA

[3] SGT Inc, Greenbelt, MD USA

[4] Inst Space & Astronaut Sci, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229, Japan

[5] Meisei Elect Co Ltd, Isesaki, Japan

[6] Univ Maryland, College Pk, MD 20742 USA

[7] Millenium Engn, Arlington, VA USA

[8] NASA, Marshall Space Flight Ctr, Huntsville, AL USA

[9] Oak Ridge Associated Univ, Oak Ridge, TN USA

[10] Orbital Sci Corp, Beltsville, MD USA

[11] Stellar Solut Inc, Chantilly, VA USA

[12] Inst Res Astrophys & Planetol, Toulouse, France

[13] Northrup Grumman, Hyattsville, MD USA

[14] Florez Engn LLC, Laurel, MD USA

[15] MEI Technol, Houston, TX USA

[16] Global Programming Solut, Fairfax, VA USA

[17] Catholic Univ Amer, Washington, DC 20064 USA

[18] Johns Hopkins Appl Phys Lab, Laurel, MD USA

[19] ASRC AS & D Inc, Beltsville, MD USA

[20] Jacobs ESSSA Grp, Huntsville, AL USA

[21] Prototype Prod Inc, Ashburn, VA USA

[22] Ares Tech Serv Corp, Greenbelt, MD USA

[23] Bandwidth Solut Inc, Mclean, VA USA

[24] Hammers Co, Greenbelt, MD USA

[25] Siena Coll, Loudonville, NY USA

[26] Space Power Elect Inc, Kathleen, GA USA

[27] Teledyne Brown Engn Inc, Huntsville, AL 35807 USA

[28] NASA Headquarders, Washington, DC USA

[29] YS Design, Tokyo, Japan

[30] Vantage Syst Inc, Lanham, MD USA

[31] Design Amer Inc, College Pk, MD USA

[32] Global Sci & Technol Inc, Greenbelt, MD USA

[33] Jackson & Tull, Greenbelt, MD USA

来源：

SPACE SCIENCE REVIEWS | 2016年 / 199卷 / 1-4期

关键词：

Magnetospheric Multiscale; Magnetic reconnection; Particle instrumentation; Electron spectrometer; Ion spectrometer; Instrument characterization and calibration; MICROCHANNEL PLATE; ION DETECTION; ELECTRON; SPACECRAFT; EFFICIENCY; ANALYZER;

D O I：

10.1007/s11214-016-0245-4

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The Fast Plasma Investigation (FPI) was developed for flight on the Magnetospheric Multiscale (MMS) mission to measure the differential directional flux of magnetospheric electrons and ions with unprecedented time resolution to resolve kinetic-scale plasma dynamics. This increased resolution has been accomplished by placing four dual 180-degree top hat spectrometers for electrons and four dual 180-degree top hat spectrometers for ions around the periphery of each of four MMS spacecraft. Using electrostatic field-of-view deflection, the eight spectrometers for each species together provide 4pi-sr field-of-view with, at worst, 11.25-degree sample spacing. Energy/charge sampling is provided by swept electrostatic energy/charge selection over the range from 10 eV/q to 30000 eV/q. The eight dual spectrometers on each spacecraft are controlled and interrogated by a single block redundant Instrument Data Processing Unit, which in turn interfaces to the observatory's Instrument Suite Central Instrument Data Processor. This paper describes the design of FPI, its ground and in-flight calibration, its operational concept, and its data products.

引用

页码：331 / 406

页数：76

共 27 条

[1] INTEGRATED DEVELOPMENT FACILITY FOR THE CALIBRATION OF LOW-ENERGY CHARGED-PARTICLE FLIGHT INSTRUMENTATION [J].