2026-09-19T12:53:30Zhttps://dspace.mit.edu/server/oai/requestoai:dspace.mit.edu:1721.1/353402022-01-13T07:54:11Zcom_1721.1_7582com_1721.1_7581col_1721.1_131023
Walter M. Hollister.
Russ, David Phillip
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
2007-01-10T15:50:55Z
2007-01-10T15:50:55Z
1988
1988
http://hdl.handle.net/1721.1/35340
19283930
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.
Includes bibliographical references.
by David Phillip Russ.
M.S.
70 leaves
2523039 bytes
2695403 bytes
application/pdf
application/pdf
eng
Massachusetts Institute of Technology
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.
http://dspace.mit.edu/handle/1721.1/7582
Aeronautics and Astronautics.
Analysis of a heavy lift launch vehicle design using small liquid rocket engines
Thesis
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