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Very High Isp Thruster with Anode Layer (VHITAL): An OverviewThis article describes the two stage bismuth fueled Hall thruster technology that was developed at TsNIIMASH [1] and the Very High Isp Thruster with Anode Layer (VHITAL) technology assessment program that is funded by NASA Exploration Systems Mission Directorate (ESMD)' Prometheus program. The overall objective of this program is to evaluate the potential for this Russian-developed thruster technology to enable near-term, Nuclear Electric Propulsion (NEf)-enabled ESMD missions to the outer planets. This 2.5 year program will provide the technology basis for the development of even higher power anode layer thrusters for rapid outer planet exploration missions and, ultimately, human exploration of the solar system. The first 6 month phase is currently in progress. If this phase is successful, the second (1 year) and third (1 year) phase of the proposed program will follow.
Document ID
20070034956
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Marrese-Reading, Colleen M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Frisbee, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sengupta, Anita
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cappelli, Mark A.
(Stanford Univ. Stanford, CA, United States)
Tverdoklebov, Sergey
(Central Research Inst. of Machine Building Korolev, Russian Federation)
Semenkin, Sasha
(Central Research Inst. of Machine Building Korolev, Russian Federation)
Boyd, Iain
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
August 24, 2013
Publication Date
September 28, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: AIAA Space 2004
Location: San Diego, CA
Country: United States
Start Date: September 28, 2004
End Date: September 30, 2004
Distribution Limits
Public
Copyright
Other
Keywords
Hall thrusters
bismuth

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