Aerospace Engineering Department
BS in Aerospace Engineering
David B. Esposto
This report details the research, design, construction, and testing of a pyrotechnic shock simulation apparatus for spacecraft applications. The apparatus was developed to be used in the Space Environments Lab at California Polytechnic State University. It will be used for testing spacecraft components with dimensions up to 24”x12”x12” as well as CubeSats. Additionally, it may be used as an instructional or demonstrational tool in the Aerospace Department’s space environments course. The apparatus functions by way of mechanical impact of an approximately 20 lb stainless steel swinging hammer. Tests were performed to verify the simulator’s functionality. Suggestions for improvement and further progress are also given.
Acoustics, Dynamics, and Controls Commons, Aeronautical Vehicles Commons, Engineering Physics Commons, Navigation, Guidance, Control and Dynamics Commons, Other Aerospace Engineering Commons, Other Mechanical Engineering Commons, Other Physics Commons, Space Vehicles Commons, Structures and Materials Commons