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Title: A study of cylindrical Hall thruster for low power space applications

Abstract

A 9 cm cylindrical thruster with a ceramic channel exhibited performance comparable to the state-of-the-art Hall thrusters at low and moderate power levels. Significantly, its operation is not accompanied by large amplitude discharge low frequency oscillations. Preliminary experiments on a 2 cm cylindrical thruster suggest the possibility of a high performance micro Hall thruster.

Authors:
; ; ;
Publication Date:
Research Org.:
Princeton Plasma Physics Lab. (PPPL), Princeton, NJ (United States)
Sponsoring Org.:
USDOE Office of Energy Research (ER) (US)
OSTI Identifier:
759246
Report Number(s):
PPPL-3479
TRN: AH200025%%41
DOE Contract Number:  
AC02-76CH03073
Resource Type:
Technical Report
Resource Relation:
Other Information: PBD: 27 Jul 2000
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; THRUSTERS; HALL EFFECT; PERFORMANCE; PROPULSION SYSTEMS; SPACE FLIGHT

Citation Formats

Raitses, Y, Fisch, N J, Ertmer, K M, and Burlingame, C A. A study of cylindrical Hall thruster for low power space applications. United States: N. p., 2000. Web. doi:10.2172/759246.
Raitses, Y, Fisch, N J, Ertmer, K M, & Burlingame, C A. A study of cylindrical Hall thruster for low power space applications. United States. https://doi.org/10.2172/759246
Raitses, Y, Fisch, N J, Ertmer, K M, and Burlingame, C A. 2000. "A study of cylindrical Hall thruster for low power space applications". United States. https://doi.org/10.2172/759246. https://www.osti.gov/servlets/purl/759246.
@article{osti_759246,
title = {A study of cylindrical Hall thruster for low power space applications},
author = {Raitses, Y and Fisch, N J and Ertmer, K M and Burlingame, C A},
abstractNote = {A 9 cm cylindrical thruster with a ceramic channel exhibited performance comparable to the state-of-the-art Hall thrusters at low and moderate power levels. Significantly, its operation is not accompanied by large amplitude discharge low frequency oscillations. Preliminary experiments on a 2 cm cylindrical thruster suggest the possibility of a high performance micro Hall thruster.},
doi = {10.2172/759246},
url = {https://www.osti.gov/biblio/759246}, journal = {},
number = ,
volume = ,
place = {United States},
year = {Thu Jul 27 00:00:00 EDT 2000},
month = {Thu Jul 27 00:00:00 EDT 2000}
}