dc.contributor.advisor | Manuel Martinez-Sanchez. | en_US |
dc.contributor.author | Robertson, Darrel Kim, 1974- | en_US |
dc.date.accessioned | 2010-01-07T20:34:13Z | |
dc.date.available | 2010-01-07T20:34:13Z | |
dc.date.copyright | 1998 | en_US |
dc.date.issued | 1998 | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.1/50388 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998. | en_US |
dc.description | Includes bibliographical references (p. 158-162). | en_US |
dc.description.statementofresponsibility | by Darrel Kim Robertson. | en_US |
dc.format.extent | 162 p. | en_US |
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 | en_US |
dc.subject | Aeronautics and Astronautics | en_US |
dc.title | A two-dimensional, non-equilibrium numerical model of an alkali seeded hydrogen arcjet thruster | en_US |
dc.type | Thesis | en_US |
dc.description.degree | M.S. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 40170151 | en_US |