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Air STAR Beyond Visual Range UAS Description and Preliminary Test ResultsThe NASA Airborne Subscale Transport Aircraft Research Unmanned Aerial System project's capabilities were expanded by updating the system design and concept of operations. The new remotely piloted airplane system design was flight tested to assess integrity and operational readiness of the design to perform flight research. The purpose of the system design is to improve aviation safety by providing a capability to validate, in high-risk conditions, technologies to prevent airplane loss of control. Two principal design requirements were to provide a high degree of reliability and that the new design provide a significant increase in test volume (relative to operations using the previous design). The motivation for increased test volume is to improve test efficiency and allow new test capabilities that were not possible with the previous design and concept of operations. Three successful test flights were conducted from runway 4-22 at NASA Goddard Space Flight Center's Wallops Flight Facility.
Document ID
20160010790
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cunningham, Kevin
(NASA Langley Research Center Hampton, VA, United States)
Cox, David E.
(NASA Langley Research Center Hampton, VA, United States)
Foster, John V.
(NASA Langley Research Center Hampton, VA, United States)
Riddick, Stephen E.
(NASA Langley Research Center Hampton, VA, United States)
Laughter, Sean A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 1, 2016
Publication Date
January 4, 2016
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-23006
Meeting Information
Meeting: 2016 AIAA SciTech Conference
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 330693.04.80.07.09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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