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Development of an In-Flight-Deployable Micro-UAV
A micro-UAV system was developed to be deployed from a host aircraft at normal jet cruise conditions (between 25,000 and 35,000 feet altitude and Mach 0.8) using the standard MJU-10/B countermeasure flare form factor. The ...
Design and Performance of an Adaptable Aircraft Manufacturing Concept
In conventional “vehicle-focused” aircraft design and manufacturing, aircraft are optimized for a given mission and then manufactured using custom-built tooling. This strategy ensures the highest vehicle performance for ...