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

Kilpatrick, Philip Stark

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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