| dc.contributor.advisor | Laurence R. Young. | en_US |
| dc.contributor.author | Kilpatrick, Philip Stark | en_US |
| dc.date.accessioned | 2014-01-09T19:43:43Z | |
| dc.date.available | 2014-01-09T19:43:43Z | |
| dc.date.issued | 1966 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/83674 | |
| dc.description | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. | en_US |
| dc.description | Lacking p.35 and p.36. | en_US |
| dc.description | Bibliography: p. 45. | en_US |
| dc.format.extent | x, 94 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 | Bending mode acceleration influence on pilot control of flexible booster dynamics. | 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 | 26019426 | en_US |
