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A study of a cylindrical, pulsed, solid fuel microthruster.

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dc.contributor.advisor Albert Solbes. en_US
dc.contributor.author Seeglitz, William Grant en_US
dc.date.accessioned 2005-08-15T23:06:34Z
dc.date.available 2005-08-15T23:06:34Z
dc.date.issued 1973 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/12368
dc.description Thesis (E.A.A.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973. en_US
dc.description Lacking leaf 30. en_US
dc.description Includes bibliographical references. en_US
dc.format.extent 175 leaves en_US
dc.format.extent 8676762 bytes
dc.format.extent 8676522 bytes
dc.format.mimetype application/pdf
dc.format.mimetype application/pdf
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. en_US
dc.rights.uri http://dspace.mit.edu/handle/1721.1/7582
dc.subject Aeronautics and Astronautics en_US
dc.title A study of a cylindrical, pulsed, solid fuel microthruster. en_US
dc.type Thesis en_US
dc.description.degree E.A.A. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics en_US
dc.identifier.oclc 29228885 en_US


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