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

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