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Electrostatic propulsion using C60 moleculesAn evaluation is made of the potential benefits of C60 molecules as a basis for ion propulsion. Because C60 is storable, its use may result in a larger usable propellant fraction than previous methods of cluster ion propulsion. C60 may also relax such engineering constraints as grid spacing, which restrict the performance of noble gas ion propulsion. The behavior of C60 in a plasma discharge environment, as well as various electron impact cross sections of the molecule, will greatly afftect the feasibility of the concept.
Document ID
19930030527
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Leifer, Stephanie D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rapp, Donald
(JPL Pasadena, CA, United States)
Saunders, Winston A.
(California Inst. of Technology Pasadena, United States)
Date Acquired
August 15, 2013
Publication Date
December 1, 1992
Publication Information
Publication: Journal of Propulsion and Power
Volume: 8
Issue: 6
ISSN: 0748-4658
Subject Category
Spacecraft Propulsion And Power
Accession Number
93A14524
Distribution Limits
Public
Copyright
Other

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