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Development overview of foreign multimode Hall electric propulsion technology and corresponding inspiration(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2014年02期
Page:
1-6
Research Field:
专论与综述
Publishing date:

Info

Title:
Development overview of foreign multimode Hall electric propulsion technology and corresponding inspiration
Author(s):
HANG Guan-rong;  KANG Xiao-lu
Shanghai Institute of Space Propulsion, Shanghai 201112, China
Keywords:
multi
PACS:
V439+.4-34
DOI:
-
Abstract:
Multimode Hall electric propulsion with good throttle capability can operate with different modes, and has obvious advantages compared to the one-mode Hall electric propulsion which has been used extensively since 1980s. Multimode Hall electric propulsion is studied and used widely because of its good adaptability to many kinds of missions such as orbit transferring and on-orbit station keeping of GEO satellites, primary propulsion of deep space crafts and spaceships, etc. The current status and development trends of foreign multimode Hall electric propulsion result in an important inspiration to the development of domestic multimode Hall electric propulsion. According to the urgent demand of electric propulsion for domestic spacecrafts, the gains of applying multimode Hall electric propulsion is analyzed quantitatively, and the development suggestion of domestic multimode Hall electric propulsion is put forward.

References:

[1]DUCHEMIN O, DUMAZERT P, CARICHON S, et al. Performance and lifetime predictions by testing and mo- deling for the PPS 5000 Hall thruster, AIAA-2003-4555 [R]. USA: AIAA, 2003.
[2]COREY R L, GASCON N, DELGADO J J. Performance and evolution of stationary plasma thruster electric propulsion for large communications satellites, AIAA-2010- 8688[R]. USA: AIAA, 2010.
[3]HOFER R R. High-specific impulse operation of the BPT-4000 Hall thruster for NASA science missions, AIAA-2010-6623[R]. USA: AIAA, 2010.
[4]GRYS K D, FISHER J, WILSON F, et al. 4.5 kW Hall thruster system qualification status, AIAA-2004-3603[R]. USA: AIAA, 2004.
[5]WITZBERGER K, MANZELLA D. Performance of solar electric powered deep space missions using hall thruster propulsion, AIAA-2005-4268[R]. USA: AIAA, 2005.
[6]KAMHAWI H, HAAG T, PINERO L. Overview of the development of a low cost high voltage Hall accelerator propulsion system for NASA science missions, AIAA- 2011-5520 [R]. USA: AIAA, 2011.
[7]FLORENZ R, GALLIMORE A D, PETERSON P Y. Developmental status of a 100-kW class laboratory nested channel Hall thruster, IEPC-2011-246[R]. [S.l.]: IEPC, 2011.
[8]AKIMOV V N, BAIDAKOV S G, GALAYKO V N. Development of KM-5 HALL effect thruster and its flight testing onboard GEO spacecraft “EXPRESS-A4”[J]. Progress in Propulsion Physics, 2009 (1): 411-424.
[9]CORNU N, MARCHANDISE F, DARNON F, et al. The PPS 1350-G qualification demonstration: 10500 hrs on the ground and 5000 hrs in flight, AIAA-2007-5197[R]. USA: AIAA, 2007.
[10]KOCH N, HARMANN H-P, KORNFELD G. Status of the THALES high efficiency multi stage plasma thruster development for HEMP-T 3050 and HEMP-T 30250, IEPC-2007-110[R]. [S.l.]: IEPC, 2007.

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