Plasma Analyzer for Measuring Spacecraft Floating Potential in LEO and GEO

被引:4
|
作者
Goembel, Luke [1 ]
机构
[1] Goembel Instruments, Baltimore, MD 21239 USA
基金
美国国家航空航天局;
关键词
Electron optics; space technology; spectroscopy; AMBIENT PHOTOELECTRON-SPECTRUM; AE-E MEASUREMENTS; ATMOSPHERE EXPLORER; TRANSPORT;
D O I
10.1109/TPS.2011.2171509
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
A design for a plasma analyzer for measuring spacecraft floating potential is described. The proposed Plasma Analyzer for Space Science (PASS) would use two methods simultaneously to determine spacecraft charge. Floating potential to kilovolts negative may be determined by the energy analysis of positively charged particles (ions) through the low energy ion cutoff method. Floating potentials from a few tens of volts negative to the highest positive potentials expected may be measured though the electron-spectroscopic method. The use of two charge-sensing techniques should allow a large range of both positive and negative floating potentials to be measured. The simultaneous use of two dissimilar methods enables the refinement of both methods and should improve the reliability of spacecraft floating potential measurement. PASS should be able to determine spacecraft floating potential in both low Earth orbit and geosynchronous Earth orbit from -10 kV to the largest positive floating potential expected. Based on what was learned from the development of the Spacecraft Charge Monitor, PASS should have superior performance in energy resolution, geometric factor, and data-gathering efficiency compared to charged particle energy analyzers that have been used in the past.
引用
收藏
页码:155 / 166
页数:12
相关论文
共 50 条
  • [2] OVERVIEW OF BATTERY USAGE IN NASA/GSFC LEO AND GEO SPACECRAFT
    YI, TY
    SPACE ELECTROCHEMICAL RESEARCH AND TECHNOLOGY ( SERT ) 1989, 1989, 3056 : 1 - 3
  • [3] Spacecraft floating potential measurements for the Wind spacecraft
    NASA Goddard Space Flight Center, Heliophysics Science Division, Greenbelt
    MD, United States
    不详
    CA
    94720-7450, United States
    arXiv, 1600,
  • [4] Spacecraft Floating Potential Measurements for the Wind Spacecraft
    Wilson, Lynn B.
    Salem, Chadi S.
    Bonnell, John W.
    ASTROPHYSICAL JOURNAL SUPPLEMENT SERIES, 2023, 269 (02):
  • [5] SPACECRAFT FORMATION DESIGN FOR BISTATIC SAR WITH GEO ILLUMINATOR AND LEO RECEIVER
    Lu, Zheng
    Wang, Yuekun
    Xu, Mingming
    Zhu, Yu
    Jian, Liang
    Li, Zhenfang
    IGARSS 2018 - 2018 IEEE INTERNATIONAL GEOSCIENCE AND REMOTE SENSING SYMPOSIUM, 2018, : 4451 - 4454
  • [6] Master 99 and in-situ spacecraft measurements: Test comparisons in LEO and GEO
    McDonnell, JAM
    Catling, DJ
    Carey, WC
    PROCEEDINGS OF THE THIRD EUROPEAN CONFERENCE ON SPACE DEBRIS, VOLS 1 AND 2, 2001, 473 : 153 - 162
  • [7] MAGNETOSPHERIC PLASMA ANALYZER FOR SPACECRAFT WITH CONSTRAINED RESOURCES
    BAME, SJ
    MCCOMAS, DJ
    THOMSEN, MF
    BARRACLOUGH, BL
    ELPHIC, RC
    GLORE, JP
    GOSLING, JT
    CHAVEZ, JC
    EVANS, EP
    WYMER, FJ
    REVIEW OF SCIENTIFIC INSTRUMENTS, 1993, 64 (04): : 1026 - 1033
  • [8] Instrument for measuring spacecraft potential
    Goembel, L
    Doering, JP
    JOURNAL OF SPACECRAFT AND ROCKETS, 1998, 35 (01) : 66 - 72
  • [9] MEASURING PLASMA TURBULENCE WITH A SPECTRUM ANALYZER
    ILIC, DB
    REVIEW OF SCIENTIFIC INSTRUMENTS, 1977, 48 (02): : 152 - 153
  • [10] MASS SAVINGS DOMAIN OF PLASMA PROPULSION FOR LEO TO GEO TRANSFER
    CHOUEIRI, EY
    KELLY, AJ
    JAHN, RG
    JOURNAL OF SPACECRAFT AND ROCKETS, 1993, 30 (06) : 749 - 754