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Design and Development of a High-Altitude, In-Flight-Deployable Micro-UAV

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dc.contributor.author Tao, Tony S.
dc.contributor.author Hansman, R. John
dc.date.accessioned 2012-06-11T16:20:46Z
dc.date.available 2012-06-11T16:20:46Z
dc.date.issued 2012-06-11
dc.identifier.uri http://hdl.handle.net/1721.1/71131
dc.description.abstract A micro-UAV system was developed to provide maximum endurance for a small atmospheric sensing payload. The system, composed of a micro-UAV and protective case, folds and fits into a MJU-10/B flare cartridge (7.1” x 2.4” x1.9”) and is designed to be ejected in-flight from altitudes up to 30,000 ft. at 300 G, to open and unfold in freefall, and to autonomously fly, sense, and transmit data for up to 45 minutes at maximum altitude. The µ UAV has a wingspan of 11.8”, a length of 6.6”, and a mass of 220grams... en_US
dc.description.sponsorship This work was funded by the MIT Lincoln Laboratory and the United States Air Force (Contract #FA8721-05-C-0002). en_US
dc.relation.ispartofseries ICAT;2012-05
dc.rights An error occurred on the license name. en
dc.rights.uri An error occurred getting the license - uri. en
dc.subject micro-UAV en_US
dc.subject atmospheric sensing en_US
dc.title Design and Development of a High-Altitude, In-Flight-Deployable Micro-UAV en_US
dc.type Technical Report en_US


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