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A performance study of a pulsed solid fuel microthruster.

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. M.S. / MICROFICHE COPY ALSO AVAILABLE IN AERO LIBRARY. / Bibliography: leaf 61. / M.S.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/13544
Date January 1969
CreatorsRadley, Roger James
ContributorsAlbert Solbes., Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Format61 leaves, 3662430 bytes, 3662190 bytes, application/pdf, application/pdf, application/pdf
RightsM.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

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