| 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 | MIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided. | 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. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 29228885 | en_US |
