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

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

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.

Bibliographic Details
Main Author:	Kilpatrick, Philip Stark
Other Authors:	Laurence R. Young.
Format:	Thesis
Language:	eng
Published:	Massachusetts Institute of Technology 2014
Subjects:	Aeronautics and Astronautics
Online Access:	http://hdl.handle.net/1721.1/83674

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