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Arcjet thruster operated with different propellants
Huang HJ(黄河激); Pan WX(潘文霞); Wu CK(吴承康)
Source PublicationIeee Transactions on Plasma Science
2011
Volume39Issue:11Pages:2934-2935
ISSN0093-3813
AbstractAbstract As a simple and reliable propulsion system, arcjet thrusters have been used in multiple satellite missions. The performance of an arcjet thruster is controlled by the characteristics of the arc-discharge behavior and the arc-electrode interactions to a large extent. The nozzle of an arcjet thruster is where the input electric energy is converted into kinetic energy. The nozzle images of an arcjet thruster operated with different propellants are presented in this paper.
DOI10.1109/TPS.2011.2155097
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Indexed BySCI ; EI
Language英语
WOS IDWOS:000299683400440
WOS Research AreaPhysics
WOS SubjectPhysics, Fluids & Plasmas
DepartmentLHD应用等离子体力学(CPCR)
ClassificationQ3
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/44580
Collection等离子体与燃烧中心(2009-2011)
Corresponding AuthorHuang HJ(黄河激)
Recommended Citation
GB/T 7714
Huang HJ,Pan WX,Wu CK. Arcjet thruster operated with different propellants[J]. Ieee Transactions on Plasma Science,2011,39(11):2934-2935
APA 黄河激,潘文霞,&吴承康.(2011).Arcjet thruster operated with different propellants.Ieee Transactions on Plasma Science,39(11),2934-2935.
MLA 黄河激,et al."Arcjet thruster operated with different propellants".Ieee Transactions on Plasma Science 39.11(2011):2934-2935.
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