Abstract
The dynamic similitude criteria for detachable sections of rocket like fairing leaf are presented. The criteria ensure the similarity of the center of mass and attitude motion of the small-scale model to the full scale body. The application of the presented criteria is illustrated by a numerical experiment. These criteria can be used to conduct small-scale experiment for the investigation of the re-entry motion of launch vehicles and its parts.
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.
