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

Internet

http://hdl.handle.net/1721.1/83674