Abstract
Analysis of internal cavity vibro-acoustic environments is one of the most critical subjects in the spacecraft development process. Accuracy and reliability of these environment predictions is important for establishing the design specifications for the payloads located within the internal cavities and designing ground tests for proper verification. This paper presents an analysis of a representative spacecraft internal cavity using Statistical Energy Analysis (SEA) and Boundary Element Method (BEM). The analysis predictions are compared to the acoustic test measurements. Observations and recommendations about test correlation and analysis limitations are also presented.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
