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Electric propulsion and controller design for drag-free spacecraft operation in low earth orbit

Thesis (M.S.)--Worcester Polytechnic Institute. / Keywords:Spacecraft; electric propulsion; LEO; GRACE; Drag-free. Includes bibliographical references (leaves 111-112).

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/85248714
Date January 2006
CreatorsMarchetti, Paul J.
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
SourceLink to electronic thesis

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