Open Access
Issue
JNWPU
Volume 42, Number 5, October 2024
Page(s) 793 - 800
DOI https://doi.org/10.1051/jnwpu/20244250793
Published online 06 December 2024
  1. BERTOLUCCI G, BARATO F, TOSON E, et al.. Impact of propulsion system characteristics on the potential for reduction of Earth observation missions at very low altitudes cost[J]. Acta Astronautica, 2020, 176: 173–191 [Article] [Google Scholar]
  2. CRISP N H, ROBERTS P C E, LIVADIOTTI S, et al. The benefits of very low Earth orbit for Earth observation missions[J]. Progress in Aerospace Sciences, 2020, 117: 100619 [Article] [CrossRef] [Google Scholar]
  3. JOSEP V L, ROBERTS P C E, ZHOU H, et al. Very low Earth orbit mission concepts for Earth observation benefits and challenges[C]//Proceedings of the 12th Reinventing Space Conference, London, 2014 [Google Scholar]
  4. DRINKWATER M R, FLOBERGHAGEN R, HAAGMANS Ret al. GOCE: ESA’s first Earth explorer core mission[J]. Space Science Reviews, 2003, 17: 419–432 [CrossRef] [Google Scholar]
  5. ZHENG P, WU J J, ZHANG Y, et al. A Comprehensive review of atmosphere-breathing electric propulsion systems[J]. International Journal of Aerospace Engineering, 2020, 2020: 8811847 [Google Scholar]
  6. NISHIYAMA K. Air breathing ion engine concept[C]//Proceedings of the 54th International Astronautical Congress of the International Astronautical Federation, Bremen, 2003 [Google Scholar]
  7. YANG Juan, MOU Hao, GENG Hai, et al.. Calculation study of electromagnetic fields and neutral particles of a wide inlet electron cyclotron resonance ion source[J]. Journal of Propulsion Technology, 2023, 44(7): 2208097 (in Chinese) [Google Scholar]
  8. JIN Yizhou, YANG Juan, FENG Bingbinget al. Ion extraction experiment for electron cyclotron resonance ion source with different magnetic topology[J]. Acta Physica Sinica, 2016, 65(4): 045201 (in Chinese) [CrossRef] [Google Scholar]
  9. TANI Y, TSUKIZAKI R, KODA D, et al. Performance improvement of the μ10 microwave discharge ion thruster by expansion of the plasma production volume[J]. Acta Astronautica, 2019, 157: 425–434 [Article] [Google Scholar]
  10. BARQUERO S, TABATA K, TSUKIZAKI R, et al.. Performance characterization of the μ10 electron-cyclotron-resonance ion thruster using alternative propellants: Krypton vs Xenon[J]. Acta Astronautica, 2023, 211: 750–754 [Article] [Google Scholar]
  11. TSUKIZAKI R, KOIZUMI H, NISHIYAMA K, et al. Measurement of axial neutral density profiles in a microwave discharge ion thruster by laser absorption spectroscopy with optical fiber probes[J]. Review of Scientific Instruments, 2011, 82(12): 123103 [Article] [CrossRef] [Google Scholar]
  12. TSUKIZAKI R, KOIZUMI H, NISHIYAMA K, et al. Plasma diagnostics inside the ECR ion thruster μ10 by laser absorption spectroscopy with optical fiber probes[C]//Proceedings of the 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Atlanta, 2012 [Google Scholar]
  13. FUNAKI I, KUNINAKA H, TOKI K. Plasma characterization of a 10 cm diameter microwave discharge ion thruster[J]. Journal of Propulsion and Power, 2004, 20(4): 718–727 [Article] [CrossRef] [Google Scholar]
  14. YANG J, FU Y L, LIU X C, et al. Bended probe diagnostics of the plasma characteristics within an ECR ion source with a rectangular waveguide[J]. Plasma Science and Technology, 2018, 20(8): 085402 [Article] [CrossRef] [Google Scholar]
  15. DEMIDOV V I, RATYNSKAIA S V, RYPDAL K. An electrostatic probe with end plugs for measurements in a magnetized plasma[J]. Review of Scientific Instruments, 1999, 70(11): 4266–4269 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  16. SHIKAMA T, KITAOKA H, HASUO M. Detection of electron energy distribution function anisotropy in a magnetized electron cyclotron resonance plasma by using a directional Langmuir probe[J]. Physics of Plasmas, 2014, 21(7): 073510 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  17. XIA X, YANG J, JIN Y Z, et al. The influence of magnetic circuit and operating parameters on the plasma property of 2 cm ECRIT ion source[J]. Vacuum, 2020, 179: 109517 [Article] [CrossRef] [Google Scholar]
  18. MOU H, JIN Y Z, YANG J, et al. Interaction between plasma and electromagnetic field in ion source of 10 cm ECR ion thruster[J]. Chinese Physics B, 2022, 31(7): 075202 [Article] [CrossRef] [Google Scholar]
  19. LIEBERMAN M A, LICHTENBERG A J. Principles of plasma discharges and materials processing[M]. New Jersey: John Wiley & Sons, 2006 [Google Scholar]
  20. DEMIDOV V I, RATYNSKAIA S V, RYPDAL K. Electric probes for plasmas: the link between theory and instrument[J]. Review of Scientific Instruments, 2002, 73(10): 3409–3439 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  21. CHEN F F. Langmuir probe analysis for high density plasmas[J]. Physics of Plasmas, 8(6): 3029–3041 [Article] [Google Scholar]
  22. JIN Yizhou, YANG Juan, LUO Litao, et al. Diagnosis of electron cyclotron resonance plasma inside ion source[J]. High Voltage Engineering, 2015, 41(9): 2950–2597 (in Chinese) [Google Scholar]
  23. GOEBEL D M, KATZ I. Fundamentals of electric propulsion: ion and hall thrusters[J]. New Jersey: John Wiley & Sons, 2008 [CrossRef] [Google Scholar]
  24. CORAL G, TSUKIZAKI R, NISHIYAMA Ket al. Microwave power absorption to high energy electrons in the ECR ion thruster[J]. Plasma Sources Science and Technology, 2018, 27(9): 095015 [Article] [CrossRef] [Google Scholar]
  25. YAMASHITA Y, TANI Y, TSUKIZAKI Ret al. Numerical investigation of plasma properties for the microwave discharge ion thruster μ10 using PIC-MCC simulation[J]. Physics of Plasmas, 2019, 26: 073510 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  26. XIA Xu, YANG Juan, JIN Yizhou, et al. Experimental study of magnetic circuit and antenna position influence on performance of 2 cm electron cyclotron resonance ion thruster[J]. Acta Physica Sinica, 68(23): 235202 (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.