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Proceedings of the Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight (3RD). Volume II. Electrical Properties of Shock-Ionized Flow Fields.

AD825617

Publication Date	1967
Personal Author	Rotman, W.; Moore, H.; Papa, R.; Lennon, J.
Page Count	356
Abstract	Contents: Research approaches to the problem of reentry communications blackout; Estimates of nonequilibrium ionization phenomena in the inviscid apollo plasma sheath; The effect of glide re-entry shock induced ionization on the communication system of the asset vehicle; The use of Langmuir probes in diagnosing ionized flow fields; Antenna breakdown in a hypersonic re-entry environment; Electromagnetic wave properties in a nonlinear, anisotropic, time-dependent plasma medium; Effects of re-entry and space environments on antenna breakdown; and A mathematical model for predicting RF interference effects in rocket exhaust plumes.
Keywords	Atmosphere entry Plasma sheaths Flow fields Symposia Electrical properties Manned spacecraft Hypersonic flight Electromagnetic radiation Space communications Ionization Thermochemistry Blackout(Propagation) Electronics High temperature Reports Abstracts Exhaust flames Apollo Plumes(Radiation)
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	46G - Plasma Physics 46H - Radiofrequency Waves 84C - Manned Spacecraft
Corporate Authors	Air Force Cambridge Research Labs L G Hanscom Field Mass
Supplemental Notes	See also Volume 1, AD-825 616.
Document Type	Technical Report
Title Note	Special repts. no. 64 (II).
NTIS Issue Number	197708

Proceedings of the Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight (3RD). Volume II. Electrical Properties of Shock-Ionized Flow Fields.

Proceedings of the Symposium on the Plasma Sheath-Plasma Electromagnetics of Hypersonic Flight (3RD). Volume II. Electrical Properties of Shock-Ionized Flow Fields.
AD825617

Publication Date	1967
Personal Author	Rotman, W.; Moore, H.; Papa, R.; Lennon, J.
Page Count	356
Abstract	Contents: Research approaches to the problem of reentry communications blackout; Estimates of nonequilibrium ionization phenomena in the inviscid apollo plasma sheath; The effect of glide re-entry shock induced ionization on the communication system of the asset vehicle; The use of Langmuir probes in diagnosing ionized flow fields; Antenna breakdown in a hypersonic re-entry environment; Electromagnetic wave properties in a nonlinear, anisotropic, time-dependent plasma medium; Effects of re-entry and space environments on antenna breakdown; and A mathematical model for predicting RF interference effects in rocket exhaust plumes.
Keywords	Atmosphere entry Plasma sheaths Flow fields Symposia Electrical properties Manned spacecraft Hypersonic flight Electromagnetic radiation Space communications Ionization Thermochemistry Blackout(Propagation) Electronics High temperature Reports Abstracts Exhaust flames Apollo Plumes(Radiation)
Source Agency	Non Paid Delimited ADS
NTIS Subject Category	46G - Plasma Physics 46H - Radiofrequency Waves 84C - Manned Spacecraft
Corporate Authors	Air Force Cambridge Research Labs L G Hanscom Field Mass
Supplemental Notes	See also Volume 1, AD-825 616.
Document Type	Technical Report
Title Note	Special repts. no. 64 (II).
NTIS Issue Number	197708