Effect of Terahertz Antenna Radiation in Hypersonic Plasma Sheaths with Different Vehicle Shapes

Author:

Zhao ZiyangORCID,Bai Bo,Yuan KaiORCID,Tang RongxinORCID,Xiong Jiawei,Wang Kaili

Abstract

Communication blackout caused by the plasma sheath surrounding hypersonic vehicles is a serious threat to the safety of hypersonic vehicles. Terahertz (THz) communication is considered to be a potential solution to the blackout problem. However, hypersonic plasma sheaths can affect not only electromagnetic wave propagation, but also the radiation performance of onboard antennae. Therefore, it is necessary to investigate the radiation performance of THz antennae in hypersonic plasma sheaths. In the present study, the impact of vehicle shapes (blunt-coned and sharp-coned vehicles) on plasma sheaths was investigated numerically. The antenna involved in the present study was a 0.14 THz array antenna. The antenna performance was compared with the aspects of mainlobe gain, mainlobe direction, and mainlobe width. The present study shows that both sharp-coned and blunt-coned plasma sheaths are inhomogeneous. Nevertheless, their structures are obviously different. Such differences yield different antenna performance in sharp-coned and blunt-coned plasma sheaths. Compared with sharp-coned plasma sheaths, blunt-coned plasma sheaths can refract antenna radiation direction, which can result in worsened communication quality in the expected direction. In addition, the phenomena are discussed in detail. Suggestions of vehicle shape design to guarantee communication quality in hypersonic flight missions are proposed.

Funder

National Natural Science Foundation of China

Interdisciplinary Innovation Fund of Natural Science from Nanchang University

Publisher

MDPI AG

Subject

Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science

Reference24 articles.

1. Hypersonic Flight

2. Progress in Reentry Communications

3. Overview of RAM reentry measurements program;Akey;NASA Spec. Publ.,1971

4. Electrostatic Probe Measurements of Plasma Surrounding Three 25,000 Foot per Second Reentry Flight Experiments;Cross,1970

5. Flight measurements of VHF-signal attenuation and antenna impedance for the RAM A-1 slender probe at velocities up to 17,800 feet per second;Sims,1963

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