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 system (measuring 49mm × 62mm × 180mm) fits in the flare canister in place of...

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Bibliographic Details
Main Authors: Tao, Tony, Hansman Jr, Robert J
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Published: American Institute of Aeronautics and Astronautics (AIAA) 2018
Online Access:http://hdl.handle.net/1721.1/114244
https://orcid.org/0000-0001-5790-0200
https://orcid.org/0000-0002-9591-3579