Accession Number : AD0825617


Title :   PROCEEDINGS OF THE SYMPOSIUM ON THE PLASMA SHEATH-PLASMA ELECTROMAGNETICS OF HYPERSONIC FLIGHT (3RD). VOLUME II. ELECTRICAL PROPERTIES OF SHOCK-IONIZED FLOW FIELDS


Descriptive Note : Special repts. no. 64 (2)


Corporate Author : AIR FORCE CAMBRIDGE RESEARCH LABS HANSCOM AFB MA


Personal Author(s) : Rotman, W ; Moore, H ; Papa, R ; Lennon, J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/825617.pdf


Report Date : May 1967


Pagination or Media Count : 359


Abstract : 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.


Descriptors :   *SYMPOSIA , *ATMOSPHERE ENTRY , *PLASMA SHEATHS , *FLOW FIELDS , ELECTRONICS , HIGH TEMPERATURE , THERMOCHEMISTRY , HYPERSONIC FLIGHT , BLACKOUT(PROPAGATION) , EXHAUST FLAMES , MANNED SPACECRAFT , SPACE COMMUNICATIONS , IONIZATION , ELECTROMAGNETIC RADIATION , REPORTS , ABSTRACTS , ELECTRICAL PROPERTIES


Subject Categories : Plasma Physics and Magnetohydrodynamics
      Radiofrequency Wave Propagation
      Manned Spacecraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE