MEASUREMENT OF IN-FLIGHT MOTION CHARACTERISTICS OF A HIGH-G LAUNCHED FLARESTABILIZED PROJECTILE WITH ON-BOARD TELEMETRY
AffiliationU.S. Army Research Laboratory
Dynamic Science. Inc
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RightsCopyright © held by the author; distribution rights International Foundation for Telemetering
Collection InformationProceedings from the International Telemetering Conference are made available by the International Foundation for Telemetering and the University of Arizona Libraries. Visit http://www.telemetry.org/index.php/contact-us if you have questions about items in this collection.
AbstractIn pursuit to understanding the flight behavior and characterizing the stability of a flarestabilized projectile, an experiment was conducted to assess the robustness of an inertial sensor suite the size of a dime (17.5mm) by integrating to a telemetry system for recording. The system had to survive launch acceleration exceeding 25,000G’s. This is the beginning of an effort to reduce the size of telemetry systems and diagnostic devices for use in medium caliber munitions and smaller. A description of the telemetry system and subsystem will be presented along with the results.
SponsorsInternational Foundation for Telemetering