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dc.contributor.authorBrown, Nelson A.
dc.date.accessioned2021-10-08T18:44:39Z
dc.date.available2021-10-08T18:44:39Z
dc.date.issued2007-08-31
dc.identifier.urihttp://hdl.handle.net/1808/31965
dc.descriptionThesis (M.S.)--University of Kansas, Aerospace Engineering, 2007.en_US
dc.description.abstractRobotic airplanes have been proposed as a tool for surveying Mars. A Mars exploration airplane could bridge the scale and resolution gaps between orbiters and surface missions. Flight testing a prototype Mars airplane may be conducted at a very high altitude over the Earth, where the air density and temperature are representative of the conditions on Mars.

This research investigates the challenges of flight testing a Mars airplane prototype at high altitude and presents the design of a system and concept of operations that will deliver the required flight test data. The system transmits flight data to the ground via a wireless data link during the flight and records the data onboard the aircraft.

Subsystems that support the flight test system have been validated by tests on the ground and on high altitude balloons flights. Preliminary flight test data are presented to demonstrate the feasibility of this flight test operation.
en_US
dc.publisherUniversity of Kansasen_US
dc.rightsThis item is protected by copyright and unless otherwise specified the copyright of this thesis/dissertation is held by the author.en_US
dc.subjectApplied sciencesen_US
dc.titleDesign of flight test systems for an autonomous, balloon-launched demonstrator for a Mars exploration airplaneen_US
dc.typeThesisen_US
dc.thesis.degreeDisciplineAerospace Engineering
dc.thesis.degreeLevelM.S.
kusw.bibid6599336
dc.rights.accessrightsopenAccessen_US


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