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  5. Bending mode acceleration influence on pilot control of flexible booster dynamics.

Bending mode acceleration influence on pilot control of flexible booster dynamics.

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Author(s)
Kilpatrick, Philip Stark
Advisor(s)
Laurence R. Young.
Date Issued
1966
Publisher
Massachusetts Institute of Technology
Description
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
Lacking p.35 and p.36.
Bibliography: p. 45.
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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http://dspace.mit.edu/handle/1721.1/7582
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http://hdl.handle.net/1721.1/83674
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