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Review of Leading Approaches for Mitigating Hypersonic Vehicle Communications Blackout and a Method of Ceramic Particulate Injection Via Cathode Spot Arcs for Blackout MitigationVehicles flying at hypersonic velocities within the atmosphere become enveloped in a "plasma sheath" that prevents radio communication, telemetry, and most importantly, GPS signal reception for navigation. This radio "blackout" period has been a problem since the dawn of the manned space program and was an especially significant hindrance during the days of the Apollo missions. An appropriate mitigation method must allow for spacecraft to ground control and ground control to spacecraft communications through the reentry plasma sheath. Many mitigation techniques have been proposed, including but not limited to, aerodynamic shaping, magnetic windows, and liquid injection. The research performed on these mitigation techniques over the years will be reviewed and summarized, along with the advantages and obstacles that each technique will need to overcome to be practically implemented. A unique approach for mitigating the blackout communications problem is presented herein along with research results associated with this method. The novel method involves the injection of ceramic metal-oxide particulate into a simulated reentry plasma to quench the reentry plasma. Injection of the solid ceramic particulates is achieved by entrainment within induced, energetic cathode spot flows.
Document ID
20100008938
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gillman, Eric D.
(Michigan Univ. Ann Arbor, MI, United States)
Foster, John E.
(Michigan Univ. Ann Arbor, MI, United States)
Blankson, Isaiah M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
February 1, 2010
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA/TM-2010-216220
E-17194
Report Number: NASA/TM-2010-216220
Report Number: E-17194
Funding Number(s)
WBS: WBS 432938.11.01.03.02.02.14
Distribution Limits
Public
Copyright
Public Use Permitted.
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