1Starkey R P. Non-equilibrium plasma effects on teleme try considerations for air-breathing hypersonic vehicle design,AIAA 2004-333[R].Washington,DC:AIAA,2004.
2Gillman E D,Foster J E,Blankson I M. Review of leading approaches for mitigating hypersonic vehicle communications blackout and a method of ceramic particulate injection via cathode spot arcs for blackout mitigation,NASA/TM 2010-216220[R].Washington,DC:NASA,2010.
3Rybak J P,Churchill R J. Progress in reentry communications[J].IEEE Transactions on Aerospace and Electronic Systems,1971,(05):879-894.
5Marabito D. The spacecraft communications blackout problem encountered during passage or entry of planetary atmosphere,IPN progress report 42-150[OL].http://ipnpr.jpl.nasa.gov/progress_report/42-150/150C.pdf,2013.
7Belov I F. Investigation of remote antenna assembly for radio communication with reentry vehicle[J].Journal of Spacecraft and Rockets,2001,(02):249-256.
8Hartunian R A. Cause and mitigation of radio frequency(RF) blackout during reentry of reusable launch vehicles.ATR 2007(5309)-1[R].El Segundo,CA:The Aerospace Corporation,2007.
9Hodara H. The use of magnetic field in the elimination of the reentry radio blackout[J].Proceedings of the IRE,1961,(12):1825-1830.
10Garg P,Dodiyal A K. Reducing RF blackout during reentry of reusable launch vehicle,AEL 4839379[A].New York:IEEE Press,2009.