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SPACE DIVISION CHRYSLER
CORPORATION

in conjunction with MSFC's Low Gravity Drop Facility. Other areas of activity have in
eluded: methods of predicting vehicle response to unsteady aerodynamic loadings (buffeting),
aerodynamic design of a recoverable reentry data return vehicle, aerodynamic design of a
recoverable booster, prediction of aerodynamic stability parameters for slow speed, wire-
guided missiles, and study of the interference effects of a jet discharging transversely to
a stream flow.

Before joining Chrysler, Mr. Vaughn worked for three years at General Dynamics,
Fort Worth Division, as a Wind Tunnel Test Engineer. This experience included all phases
of wind tunnel work, from test scheduling to final report writing.

Publications

Development of an Air Facility for the Investigation of Flow Conditions that Exist in
the Base Region of the Saturn Booster During Launch. MTP-AERO-61-37, April 1961.

Cold Flow Studies of a Launcher for the C-5 Vehicle. Part I, II & III, M-AERO-E-
112-62, M-AERO-E-211-62, M-AERO-E-133-63.

Modified Newtonian Flow Theory, Chrysler TR HSM-R091, January 1965.

Simulation of a Facility for Zero and Low Gravity Environments, Chrysler TR HSM-
R-32-67, May, 1967.

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