| dc.contributor.advisor | Manuel Martinez-Sanchez. | en_US |
| dc.contributor.author | Miller, Scott Alan, 1966- | en_US |
| dc.date.accessioned | 2005-08-16T19:38:26Z | |
| dc.date.available | 2005-08-16T19:38:26Z | |
| dc.date.copyright | 1994 | en_US |
| dc.date.issued | 1994 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/12205 | |
| dc.description | Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994. | en_US |
| dc.description.statementofresponsibility | by Scott Alan Miller. | en_US |
| dc.format.extent | 274 p. | en_US |
| dc.format.extent | 19565003 bytes | |
| dc.format.extent | 19564761 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 | Multifluid nonequilibrium simulation of arcjet thrusters | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | Sc.D. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 30679887 | en_US |
