Structure and Materials Aspects of the Prime Flight Test Vehicle
Buckling and Steady Flutter of Heat-Compressed Panels in a Supersonic Flow
Apollo LEM adapter structural analysis Final report, Jan. 1965 - Apr. 1966
Reliability Analyses of Modular Power Conditioning and Control Systems for Ion Engines Final Report
Theory of thermal similitude with applications to spacecraft - A survey.
Solid Propellant Rocket Motor Performance Computer Programs Using the Group Transformation Method