5,517 research outputs found

    Synthesis Technique of Thickness-Customizable Multilayered Frequency Selective Surface for Plasma-Based Electromagnetic Structures

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    This dissertation provides a synthesis technique for the design of thickness-customizable high-order (N โ‰ฅ 2) bandpass frequency selective surface (FSS) and its application in realizing versatile multi-layered FSS and absorbers. Admittance inverters layers are used to synthesize the transfer response of the filter given desired characteristics such as filter type, center frequency, and bandwidth. These inverter layers are essentially electromagnetic coupling interlayers that can be adjusted to customize the thickness of multilayered FSS without degrading the desired filter performance. A generalized equivalent circuit model is used to provide physical insights of the proposed design. This synthesis technique is adopted to deliver a versatile implementation capability of high-order FSS filters using various dielectric spacers with arbitrary thicknesses. Such technique enables the realization of spatial filters with variable size, while maintaining the desired filter response. To highlight the significance of the proposed synthesis technique, its concept is applied to two practical problems including the design of compact switchable FSS and adaptive/tunable microwave absorbers as it may allow simpler integration of active components that require specific physical dimensions. In the first practical problem, the feasibility of deploying plasma switchable compact spatial filter in harsh electromagnetic radiation environments is investigated. The proposed FSS integrates contained plasma (plasma-shells) as active tuning elements. These ceramic, gas-encapsulating shells are ideal for high-power microwave and electromagnetic pulse protection because they are rugged, hermetic, operable at extreme temperatures, and insensitive to ionizing radiation. A 2D periodic second-order switchable spatial filter is implemented. It is composed of electrically small Jerusalem cross structures embedded with discrete plasma shells strategically located to effectively switch the transfer function of the filter. This technique is used to realize compact low profile second order band pass spatial filter operating at S-band. It also has the ability to switch its transfer function within 20 to 100 ns while enabling in-band shielding protection for aerospace or terrestrial electromagnetic systems subjected to high power microwave energy (HPME) and high electromagnetic pulse (HEMP) in harsh space environment. Experimental results are shown to be in good agreement with simulation results. The second practical problem is addressed by deploying a large-scale adaptable compressed Jaumann absorber for harsh and dynamic electromagnetic environments. The multilayered conductor-backed absorbers are realized by integrating ceramic gas-encapsulating shells and a closely coupled resonant layer that also serves as a biasing electrode to sustain the plasma. These active frequency selective absorbers are analyzed using a transmission line approach to provide the working principle and its frequency tuning capability. By varying the voltage of the sustainer, the plasma can be modeled as a lossy, variable, frequency-power-dependent inductor, providing a dynamic tuning response of the absorption spectral band. To study the power handling capability of the tunable absorber, dielectric and air breakdowns within the device are numerically emulated using electromagnetic simulation by quantifying the maximum field enhancement factor (MFEF). Furthermore, a comprehensive thermal analysis using a simulation method that couples electromagnetics and heat transfer is performed for the absorber under high power continuous microwave excitations. The maximum power level handling capability of the microwave absorber has been numerically predicted and validated experimentally

    Quasi-coherent thermal emitter based on refractory plasmonic materials

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    The thermal emission of refractory plasmonic metamaterial - a titanium nitride 1D grating - is studied at high operating temperature (540 {\deg}C). By choosing a refractory material, we fabricate thermal gratings with high brightness that are emitting mid-infrared radiation centered around 3 ฮผ\mum. We demonstrate experimentally that the thermal excitation of plasmon-polariton on the surface of the grating produces a well-collimated beam with a spatial coherence length of 32{\lambda} (angular divergence of 1.8{\deg}) which is quasi-monochromatic with a full width at half maximum of 70 nm. These experimental results show good agreement with a numerical model based on a two-dimensional full-wave analysis in frequency domain.Comment: 10 pages, 5 figure

    ์‚ฐ์†Œ ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ •์„ ์ด์šฉํ•œ ์‘๋ ฅ ๊ตฌ๋ฐฐ MEMS ์™ธํŒ”๋ณด๊ฐ€ ์žˆ๋Š” Ka๋ฐด๋“œ ๋Œ€์—ญ ๊ฐ€๋ณ€ํ˜• ๋ฉ”ํƒ€๋ฌผ์งˆ ํก์ˆ˜์ฒด

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    ํ•™์œ„๋…ผ๋ฌธ(๋ฐ•์‚ฌ) -- ์„œ์šธ๋Œ€ํ•™๊ต๋Œ€ํ•™์› : ๊ณต๊ณผ๋Œ€ํ•™ ์ „๊ธฐยท์ •๋ณด๊ณตํ•™๋ถ€, 2022. 8. ๊น€์šฉ๊ถŒ.This dissertation proposes and realizes the first Ka-band frequency tunable metamaterial absorber with stress-induced MEMS cantilever with oxygen plasma ashing process. To employ a MEMS-driven actuator for LC resonance frequency tuning method in the GHz regime, the split-ring resonator (SRR) structure of the metamaterial unit cell is designed to have a sub-mm scale cantilever as a capacitor element of the unit cell. To enlarge capacitance change, the MEMS cantilever is released with a large out-of-plane deflection by the plasma ashing process. This MEMS cantilever with stress gradient is arranged at four parts of a symmetrical SRR unit cell, and the two cells compose the absorber sample as an array structure. The overall cantilevers of the absorber actuate from the initial bent upward state to pulled down state when the electrostatic voltage is applied. The decrease of deflection reduces the gap between cantilevers and bottom electrodes to increase capacitance for frequency tuning to lower frequency. To verify and improve the uniformity of the mechanical behavior of the absorber, this research proposes and demonstrates 3 different design types of releasing on stress-induced cantilevers. First, the array design of 12 cantilevers with 400 ฮผm in length and 50 ฮผm widths is modified from a cantilever with 400 ฮผm in length and 800 ฮผm widths. To overcome the limitation on the mechanical behavior of cantilever arrays due to their nonuniformity, further modification on etching hole rearrangement is reflected in the 2nd type of rectangular cantilever. The space length of etch hole varies depending on the position from the open end of cantilevers. This incremental space length between 8 ฮผm etch holes from the open end enables sequential releasing of cantilevers during photoresist oxygen plasma ashing. The cyclic process was performed in the ashing process to lower the distribution of fabrication results. Finally, the last design to have a semicircle shape with incremental space length between etching holes to improve the uniformity of the cantilever to prevent such drawbacks of a wrinkled profile which the previous design shows. Also, our last design is driven by a digital drive creating 5 different reconfiguration states. With full-wave simulations, the performance of the proposed absorber demonstrates experimentally in each of 5 different reconfiguration states. The initially measured deflection of the cantilever beam is 51.8 ฮผm on average. At the initial state, the resonant frequency and the absorptivity are 32.95 GHz and 80.95%. When all the cantilevers are pulled down, the frequency shifts a total of 4.08 GHz from the initial state showing a tuning ratio of 12.29 %. The error between the measured value and the simulation value came within 0.39 GHz in all five states. This dissertation demonstrated the potential of MEMS as a tuning method for Ka-band absorbers.์ด ๋…ผ๋ฌธ์€ ์‚ฐ์†Œ ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ •์„ ์‚ฌ์šฉํ•˜์—ฌ ์‘๋ ฅ๊ตฌ๋ฐฐ MEMS ์™ธํŒ”๋ณด๋ฅผ ์‚ฌ์šฉํ•œ ์ตœ์ดˆ์˜ Ka ๋Œ€์—ญ ์ฃผํŒŒ์ˆ˜ ๊ฐ€๋ณ€ ๋ฉ”ํƒ€๋ฌผ์งˆ ํก์ˆ˜์ฒด๋ฅผ ์ œ์•ˆํ•˜๊ณ  ๊ฒ€์ฆํ•˜์˜€๋‹ค. GHz ์˜์—ญ์—์„œ LC ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜ ๊ฐ€๋ณ€ ๋ฐฉ์‹์— MEMS ์•ก์ถ”์—์ดํ„ฐ๋ฅผ ๊ตฌ๋™ํ•˜๊ธฐ ์œ„ํ•ด ๋ฉ”ํƒ€๋ฌผ์งˆ ๋‹จ์œ„ ์…€์ธ ๋ถ„ํ• ๋ง๊ณต์ง„๊ธฐ ๊ตฌ์กฐ๋Š” mm ์Šค์ผ€์˜ ์™ธํŒ”๋ณด๋ฅผ ์ •์ „์šฉ๋Ÿ‰์˜ ์š”์†Œ๋ฅผ ๊ฐ–๋„๋ก ์„ค๊ณ„ํ•˜์˜€๋‹ค. ์ •์ „์šฉ๋Ÿ‰ ๋ณ€ํ™”๋ฅผ ์ตœ๋Œ€ํ™”ํ•˜๊ธฐ ์œ„ํ•ด MEMS ์™ธํŒ”๋ณด๋Š” ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ •์— ์˜ํ•ด ์ˆ˜์ง ๋ฐฉํ–ฅ์œผ๋กœ ํฐ ํŽธํ–ฅ์ฐจ๋ฅผ ๊ฐ–๋„๋ก ์„ค๊ณ„ํ•˜์˜€๋‹ค. ์‘๋ ฅ๊ตฌ๋ฐฐ MEMS ์™ธํŒ”๋ณด๋Š” ๋Œ€์นญ์˜ ๋ถ„ํ• ๋ง ๊ณต์ง„๊ธฐ ๊ตฌ์กฐ์˜ ๋‹จ์œ„ ์…€ 4๊ณณ์— ๋ฐฐ์—ด๋˜๊ณ  ๋‘ ์…€์€ ๋ฐฐ์—ด๊ตฌ์กฐ๋กœ ์„ค๊ณ„๋˜์—ˆ๋‹ค. ์ด ๋•Œ, ํ’€์ธ ์ „์•• ์ด์ƒ์˜ ๋†’์€ ์ „์••์„ ์ธ๊ฐ€ ์‹œ ์™ธํŒ”๋ณด๋Š” ๋ฐ”๋‹ฅ์ „๊ทน์— ๋ถ™๊ฒŒ ๋˜์–ด ์ •์ „์šฉ๋Ÿ‰์„ ํ‚ค์šฐ๊ณ  LC ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜๋ฅผ ๋‚ฎ์ถ˜๋‹ค. ํก์ˆ˜์ฒด์˜ ๊ธฐ๊ณ„์  ๊ฑฐ๋™์— ๋Œ€ํ•œ ๊ท ์ผ์„ฑ์„ ๊ฐœ์„ ํ•˜๊ธฐ ์œ„ํ•ด ์ด 3๊ฐ€์ง€ ๋‹ค๋ฅธ ๋ชจ์–‘์˜ ์™ธํŒ”๋ณด๋ฅผ ์„ค๊ณ„ํ•˜์˜€๋‹ค. ๋จผ์ € ๊ธธ์ด 400ฮผm, ๋„ˆ๋น„ 50ฮผm์ธ ์™ธํŒ”๋ณด๋ฅผ 12๊ฐœ์˜ ๋ฐฐ์—ด์ƒํƒœ๋กœ ์„ค๊ณ„ํ•˜์—ฌ ์ปดํ“จํ„ฐ ์‹œ๋ฎฌ๋ ˆ์ด์…˜๊ณผ ์ธก์ •๊ฐ’์„ ํ™•์ธํ•˜์˜€๋‹ค. ์ฒซ ๋ฒˆ์งธ ํก์ˆ˜์ฒด์˜ ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ •์„ ํ†ตํ•œ ์™ธํŒ”๋ณด ๊ตฌํ˜„ ๊ณต์ •์˜ ๊ฒฐ๊ณผ, 96๊ฐœ์˜ ์™ธํŒ”๋ณด์˜ ํ‰๊ท  ๊ฐ’์€ 41.5 ฮผm์ด๊ณ  ํ‘œ์ค€ ํŽธ์ฐจ๋Š” 15.4 ฮผm์˜€๋‹ค. ์ฒซ ๋ฒˆ์งธ ํก์ˆ˜์ฒด์˜ ๊ฒฝ์šฐ ์ œ์ž‘ ์™ธํŒ”๋ณด์˜ ์‚ฐํฌ๊ฐ€ ์ƒ๋‹นํžˆ ํผ์—๋„ ๋ถˆ๊ตฌํ•˜๊ณ , 15 V๊นŒ์ง€ ์•„๋‚ ๋กœ๊ทธ ํŠœ๋‹์„ ํ•˜์—ฌ, ์ดˆ๊ธฐ ์ƒํƒœ์˜ 28 GHz์˜ ๊ณต์ง„์ฃผํŒŒ์ˆ˜์—์„œ 25.5 GHz์˜ ๊ณต์ง„์ฃผํŒŒ์ˆ˜ ๋ณ€ํ™”ํ•˜์—ฌ ์ด 2.5 GHz์˜ ์ฃผํŒŒ์ˆ˜ ๊ฐ€๋ณ€๋ฒ”์œ„๋ฅผ ๋„๋‹ฌํ•˜์˜€๋‹ค. ๋ฐ˜์‚ฌ๊ณ„์ˆ˜๋Š” ์ดˆ๊ธฐ -5.68 dB์—์„œ -33.60 dB๊นŒ์ง€ ๋ณ€ํ™”ํ•˜์˜€๊ณ , ํˆฌ๊ณผ ๊ณ„์ˆ˜์˜ ๊ฒฝ์šฐ -40์—์„œ -60 dB๋ฅผ ์œ ์ง€ํ•˜์˜€๋‹ค. ํก์ˆ˜์œจ ๊ณ„์‚ฐ ๊ฒฐ๊ณผ, ๊ฐ ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜์—์„œ์˜ ํก์ˆ˜์œจ์€ 0 V์ผ ๋•Œ 72.9%์—์„œ ๊ณ„์† ์ฆ๊ฐ€ํ•˜๋ฉฐ 15 V์ผ๋•Œ 99.9%์˜ ํก์ˆ˜์œจ์„ ๋„๋‹ฌํ•˜์˜€๋‹ค. ๊ทธ๋Ÿผ์—๋„ ๋ถˆ๊ตฌํ•˜๊ณ , ์™ธํŒ”๋ณด ์–ด๋ ˆ์ด ๊ฐ–๋Š” ๋„“์€ ํŽธํ–ฅ๊ฐ’ ์‚ฐํฌ๊ฐ€ ์ปดํ“จํ„ฐ ์‹œ๋ฎฌ๋ ˆ์ด์…˜๊ณผ์˜ ๊ดด๋ฆฌ๊ฐ€ ์žˆ์–ด ๊ฐœ์„ ๋œ ์„ค๊ณ„๋ฅผ ๋‹ค์‹œ ์‹œ๋„ํ•˜์˜€๋‹ค. ์•ž์„  ์„ค๊ณ„์˜ ๋‹จ์ ์„ ๊ทน๋ณตํ•˜๊ธฐ ์œ„ํ•ด ์ ์ง„์ ์œผ๋กœ ์ฆ๊ฐ€ํ•˜๋Š” ํŒจํ„ด์˜ ์‹๊ฐ ๊ตฌ๋ฉ์„ ์™ธํŒ”๋ณด์— ์ ์šฉํ•˜์˜€๋‹ค. ์ด ๋‘ ๋ฒˆ์งธ ๊ตฌ์กฐ ๋˜ํ•œ ์ œ์ž‘, ์ปดํ“จํ„ฐ ๊ณ„์‚ฐ ๋ฐ ์‹คํ—˜ ๊ฒ€์ฆํ•˜์˜€๋‹ค. ์ด๋Ÿฌํ•œ ์‹๊ฐ ๊ตฌ๋ฉ ํŒจํ„ด์€ ์™ธํŒ”๋ณด๋ฅผ ์‚ฐ์†Œ ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ •์œผ๋กœ ๊ตฌํ˜„ ์‹œ, ์ œ์ž‘ ๊ท ์ผ์„ฑ์„ ํฌ๊ฒŒ ์ฆ๊ฐ€์‹œํ‚จ๋‹ค. ๋‚˜์•„๊ฐ€ ํ”Œ๋ผ์ฆˆ๋งˆ ์• ์‹ฑ ๊ณต์ • ๋˜ํ•œ ์‹œ๊ฐ„์„ ๋ถ„ํ• ํ•˜์—ฌ ์ œ์ž‘ํ•จ์œผ๋กœ์จ ๊ท ์ผ๋„๋ฅผ ํฌ๊ฒŒ ์ฆ๊ฐ€์‹œํ‚จ๋‹ค. ๋˜ํ•œ ๋‘๋ฒˆ์งธ ์„ค๊ณ„๋ถ€ํ„ฐ๋Š” ์‘๋ ฅ ๊ตฌ๋ฐฐ๋กœ ์ธํ•œ ํฐ ํŽธํ–ฅ์„ ๊ฐ–๋Š” ์™ธํŒ”๋ณด๊ฐ€ ๊ฐ–๋Š” ๋น„ํ‰ํ˜• ๊ตฌ๋™ ๋ฐฉ์‹์˜ ํ•ด์„ ์–ด๋ ค์›€์— ๋”ฐ๋ผ ์ „์••์„ ๊ฐœ๋ณ„์ ์œผ๋กœ ์ธ๊ฐ€ํ•˜๋ฉฐ on/off ํ˜•ํƒœ์˜ ๋””์ง€ํ„ธ ๊ตฌ๋™๋ฐฉ์‹์œผ๋กœ๋งŒ ๊ตฌ๋™ํ•˜๊ฒŒ๋” ์‹œ์Šคํ…œ ๊ตฌ๋™๋ฐฉ์‹์„ ๋ณ€๊ฒฝํ•˜์˜€๋‹ค. 2๊ฐœ์˜ ๋ฉ”ํƒ€๋ฌผ์งˆ ๋‹จ์œ„ ๊ตฌ์กฐ์— 4๊ฐœ์˜ ์ „๊ทน์„ ๋ถ„๋ฆฌํ•˜์—ฌ ์ด 5๊ฐœ์˜ ๊ตฌ์กฐ์ ์œผ๋กœ ๋‹ค๋ฅธ ์ƒํƒœ๋ฅผ ๊ตฌํ˜„ํ•˜์˜€๋‹ค. ๋ชจ๋“  ์™ธํŒ”๋ณด๊ฐ€ ์œ„๋กœ ํœ˜์–ด์ง„ ์ƒํƒœ์—์„œ ์ „๊ทน์— ์ „์••์„ ์ˆœ์ฐจ์ ์œผ๋กœ ์ธ๊ฐ€ํ•˜์—ฌ 2๊ฐœ์”ฉ ๋ฐ”๋‹ฅ์— ๋ถ™๊ฒŒ ํ•˜์—ฌ ์ตœ์ข…์ ์œผ๋กœ ๋ชจ๋“  ์™ธํŒ”๋ณด๊ฐ€ ๋ฐ”๋‹ฅ์— ๋ถ™๊ฒŒ ํ•˜์˜€๋‹ค. ๋‘ ๋ฒˆ์งธ ํก์ˆ˜์ฒด์˜ ๊ฒฝ์šฐ, ์™ธํŒ”๋ณด ๊ตฌํ˜„์ด ํฌ๊ฒŒ ๊ฐœ์„ ๋จ์—๋„ ๋ถˆ๊ตฌํ•˜๊ณ  ์ดˆ๊ธฐ 32.24 GHz์˜ ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜ ๊ฐ’์—์„œ 2.14 GHz๋งŒ ๋ณ€ํ™”ํ•˜์—ฌ ์ตœ์ข… 30.10 GHz์˜ ๊ณต์ง„์ฃผํŒŒ์ˆ˜ ์ธก์ • ๊ฒฐ๊ณผ๋ฅผ ๋ณด์˜€๋‹ค. ํก์ˆ˜์œจ์˜ ๊ฒฝ์šฐ์—๋„ ์ดˆ๊ธฐ 83.59%์—์„œ ์ตœ์ข… 90.75%์˜ ๊ฒฐ๊ณผ๋ฅผ ๋ณด์˜€์ง€๋งŒ ์ปดํ“จํ„ฐ ๊ณ„์‚ฐ๊ณผ ๋งŽ์€ ์ฐจ์ด๋ฅผ ๋ณด์˜€๋‹ค. ์ตœ์ข…์ ์œผ๋กœ ์•ž์„  2๊ฐœ์˜ ์„ค๊ณ„๋ฅผ ๋ณด์™„ํ•œ, ์ตœ์ข… ์ง„ํ™”ํ•œ ํ˜•ํƒœ์ธ, ๋ฐ˜์›ํ˜• ์‘๋ ฅ ๊ตฌ๋ฐฐ ์™ธํŒ”๋ณด๋ฅผ ๊ฐ–๋Š” ํก์ˆ˜์ฒด๋ฅผ ์„ค๊ณ„, ์ œ์ž‘, ๋ฐ ์‹คํ—˜ ๊ฒ€์ฆํ•˜์˜€๋‹ค. ํŠนํžˆ, ์™ธํŒ”๋ณด๊ฐ€ ๊ฐ–๋Š” ๋ถˆ์•ˆ์ •ํ•œ ๊ธฐ๊ณ„์  ๊ฑฐ๋™์„ ๋‹จ์ˆœํ™”ํ•˜์—ฌ ๋””์ง€ํ„ธ ๊ตฌ๋™์„ ํ•˜๊ฒŒ๋” ํก์ˆ˜์ฒด๋ฅผ ์„ค๊ณ„ํ•˜์˜€๋‹ค. ์‹๊ฐ ํŒจํ„ด์˜ ๊ฑฐ๋ฆฌ๋ฅผ 2 ฮผm์”ฉ ๋Š˜๋ฆฌ๋ฉฐ ๋ฐ˜์› ํ˜•ํƒœ์˜ ์™ธ๊ณฝ์œผ๋กœ๋ถ€ํ„ฐ ์„ค๊ณ„ํ•œ ๊ฒฐ๊ณผ ์žฌํ˜„์„ฑ๊ณผ ๊ท ์ผ์„ฑ์ด ๋งค์šฐ ํฌ๊ฒŒ ๊ฐœ์„ ๋˜์—ˆ๋‹ค. ํŠนํžˆ ๋ฐ˜์› ํ˜•ํƒœ์˜ ์™ธํŒ”๋ณด์˜ ๊ฒฝ์šฐ ์ตœ๊ณ ์  ํŽธํ–ฅ ๋†’์ด๊ฐ€ ํ•ญ์ƒ ๋ฐ˜์› ์ค‘๊ฐ„์—์„œ ๊ตฌํ˜„๋˜๊ธฐ ๋•Œ๋ฌธ์— ๋ฐ˜์›ํ˜• ์™ธํŒ”๋ณด ๊ฐ„์˜ ๋ชจ์–‘์ด ๊ท ์ผํ•˜๊ฒŒ ์œ ์ง€๋œ๋‹ค. ์ œ์ž‘๋œ 18๊ฐœ ํก์ˆ˜์ฒด ์ƒ˜ํ”Œ์—์„œ 144๊ฐœ์˜ ์™ธํŒ”๋ณด๋ฅผ ์ธก์ •ํ•œ ๊ฒฐ๊ณผ ํ‰๊ท  ํŽธํ–ฅ ๋†’์ด์˜ ํ‰๊ท  ๊ฐ’์ด 51.8 ฮผm์˜€์œผ๋ฉฐ ํ‘œ์ค€ ํŽธ์ฐจ๋Š” 3.1ฮผm์˜€๋‹ค. 4๊ฐœ์˜ ์ „๊ทน์—์„œ ๊ธฐ๋ฐ˜ํ•œ 5๊ฐœ ์ƒํƒœ์˜ ์„œ๋กœ ๋‹ค๋ฅธ ๊ตฌ์กฐ์— ๋”ฐ๋ฅธ ๋ฐ˜์‚ฌ ๊ณ„์ˆ˜์™€ ํˆฌ๊ณผ ๊ณ„์ˆ˜๋ฅผ ๋„ํŒŒ๊ด€ ์ธก์ •์œผ๋กœ ์‹คํ—˜ ๊ฐ’์„ ์–ป์—ˆ๋‹ค. ์ƒ์šฉ ์œ ํ•œ์š”์†Œ๋ฒ• ์ปดํ“จํ„ฐ ๊ณ„์‚ฐ๊ณผ ๋น„๊ต ๊ฒ€์ฆํ•˜์˜€๋‹ค. ์ดˆ๊ธฐ ์ƒํƒœ์—์„œ ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜๋Š” 32.95 GHz์˜€๊ณ , ๋ชจ๋“  ์™ธํŒ”๋ณด๊ฐ€ ํ’€์ธ ์ „์•• ์ธ๊ฐ€๋กœ ์ธํ•ด ๋ฐ”๋‹ฅ ์ „๊ทน์— ๋ถ™์œผ๋ฉด ํ•˜๋ฉด ์ฃผํŒŒ์ˆ˜ 28.87 GHz๊ฐ€ ๋˜์–ด ์ด 4.08GHz ์ด๋™ํ•˜์—ฌ 12.29%์˜ ์ฃผํŒŒ์ˆ˜ ๊ฐ€๋ณ€์œจ์„ ๊ฐ–๋Š”๋‹ค. ์ธก์ •๊ฐ’๊ณผ ์œ ํ•œ์š”์†Œ ์‹œ๋ฎฌ๋ ˆ์ด์…˜ ๊ฐ’์˜ ์˜ค์ฐจ๋Š” 5๊ฐœ ์ƒํƒœ ๋ชจ๋‘์—์„œ 0.39GHz ์ด๋‚ด์˜€๋‹ค. ํก์ˆ˜์œจ์˜ ๊ฒฝ์šฐ ๊ฐ ์ƒํƒœ์—์„œ 80.95 %, 88.17 %, 86.29 %, 99.21 %, and 86.51% ๊ฐ’์„ ๋ณด์˜€๋‹ค. ์ด ๋…ผ๋ฌธ์€ Ka-๋Œ€์—ญ ํก์ˆ˜์ฒด์˜ ํŠœ๋‹ ๋ฐฉ๋ฒ•์œผ๋กœ์„œ MEMS์˜ ๊ฐ€๋Šฅ์„ฑ์„ ๋ณด์—ฌ์ฃผ์—ˆ๋‹ค.CHAPTER 1. Introduction 1 1.1 Background 1 1.1.1 Advent of metamaterial 1 1.1.2 Application of metamaterial 2 1.1.3 Physics of metamaterial 3 1.1.4 Meta-atom 10 1.1.5 Electromagnetic absorber to metamaterial absorber 14 1.1.6 Reconfigurable metamaterial 17 1.1.7 MEMS reconfigurable metamaterial 21 1.1.8 Tunable metamaterial absorber 24 1.1.9 MEMS reconfigurable metamaterial absorber 27 1.1.10 Tunable metamaterial absorber for Ka-band 29 1.2 Originality and contribution 32 1.3 Document structure 33 CHAPTER 2. Stress-induced sub-mm scale cantilever 34 2.1 Initial design 34 2.2 Cantilever arrays with stress gradient 37 2.2.1 Preliminary experiment 37 2.2.2 Design 38 2.2.2 Fabrication results 39 2.3 Rectangular shape sub-mm scale cantilever with incremental etch hole spacing 40 2.3.1 Preliminary experiment 40 2.3.2 Design 42 2.4 Semicircular sub-mm scale cantilever with incremental etch hole 49 2.4.1 Design of semicircular sub-mm scale cantilever with incremental etch hole 49 2.4.2 Fabrication 52 CHAPTER 3. The 1st design of MEMS tunable metamaterial absorber with cantilever arrays for continuous tuning 57 3.1 General overview 57 3.2 Design 59 3.2.1 Split ring resonator and simulation 61 3.2.2 Capacitance of cantilever with stress gradient 64 3.2.3 Electrostatic driving of cantilever 67 3.2.4 Stress analysis & PR ashing 69 3.3 Fabrication 71 3.3.1 Fabrication process 71 3.3.2 Fabrication results 74 3.4 Simulation 77 3.5 Experiment 81 3.5.1 Experiment setup 81 3.5.2 Experiment results 84 3.6 Summary 86 CHAPTER 4. The 2nd design of MEMS tunable metamaterial absorber with rectangular shape sub-mm scale stress-induced cantilever with an incremental etch hole spacing for digital driving 87 4.1 General overview 87 4.2 Design 90 4.3 Fabrication 93 4.4 Simulation 98 4.5 Experiment 100 4.6 Summary 102 CHAPTER 5. The 3rd design of MEMS tunable metamaterial absorber with semicircular sub-mm scale stress-induced cantilever with an incremental etch hole spacing for digital driving 103 5.1 General overview 103 5.2 Design 107 5.2.1 Electromagnetic properties 107 5.2.2 Design parameter 109 5.3 Fabrication 112 5.4 Simulation 119 5.4.1 Simulation setup 119 5.4.2 Simulation results 122 5.5 Experiment 126 5.5.1 Experiment setup 126 5.5.2 Preliminary experiment 130 5.5.2 Experiment results 133 5.6 Further Analysis 137 5.6.1 The waveguide simulation 137 5.6.2 The periodic metamaterial unit cell simulation 141 5.6.3 Analysis on the surface current 148 5.7 Summary 152 5.7.1 Summary of the 1st, 2nd, and 3rd design 152 5.7.2 Comparison with MEMS tunable metamaterial absorber 155 5.7.3 Comparison with Ka-band tunable metamaterial absorber 157 CHAPTER 6. Conclusion 159 Bibliography 161 ์ดˆ๋ก (๊ตญ๋ฌธ) 180๋ฐ•

    Investigation of passive atmospheric sounding using millimeter and submillimeter wavelength channels

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    Activities within the period from July 1, 1992 through December 31, 1992 by Georgia Tech researchers in millimeter and submillimeter wavelength tropospheric remote sensing have been centered around the calibration of the Millimeter-wave Imaging Radiometer (MIR), preliminary flight data analysis, and preparation for TOGA/COARE. The MIR instrument is a joint project between NASA/GSFC and Georgia Tech. In the current configuration, the MIR has channels at 90, 150, 183(+/-1,3,7), and 220 GHz. Provisions for three additional channels at 325(+/-1,3) and 8 GHz have been made, and a 325-GHz receiver is currently being built by the ZAX Millimeter Wave Corporation for use in the MIR. Past Georgia Tech contributions to the MIR and its related scientific uses have included basic system design studies, performance analyses, and circuit and radiometric load design, in-flight software, and post-flight data display software. The combination of the above millimeter wave and submillimeter wave channels aboard a single well-calibrated instrument will provide unique radiometric data for radiative transfer and cloud and water vapor retrieval studies. A paper by the PI discussing the potential benefits of passive millimeter and submillimeter wave observations for cloud, water vapor and precipitation measurements has recently been published, and is included as an appendix

    High Power Microwave Operational Exposure Detection using Thermoacoustic Wave Generation in Lossy Dielectric Polymers

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    A feasibility analysis for the use of microwave-induced thermoacoustic (TA) wave generation in lossy dielectric media to detect pulsed high power microwave directed energy weapons in force health protection applications was conducted based on a series of empirical and computational investigations. A potential target volume material, carbon-loaded polytetrafluoroethylene, was identified for further study based on anticipated complex dielectric properties, with laboratory measurements of select electromagnetic (EM), thermal, and elastic material properties of relevance to the TA effect conducted to determine parameter values. A planar geometry TA-based signal chain model using thin film piezoelectric sensors was developed for both finite element method based numerical simulation and in-beam response testing, with TA signal output evaluated in the time and frequency domain using both approaches. Based on empirically-derived complex permittivity values, a single-term Cole-Cole dielectric relaxation model approximation was developed over the 2-110 GHz microwave frequency region to permit a more general evaluation of EM coupling efficiency of the material. Modeling and simulation of the idealized signal chain allowed the analysis of TA waveform dependency on microwave beam parameters not otherwise accessible during in-beam response testing. High frequency TA signal data was suitably fit to a pulse width sensitivity impulse response function model for the target geometry and found to be in good agreement for personnel exposure applications

    NASA patent abstracts bibliography: A continuing bibliography. Section 1: Abstracts (supplement 07)

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    This bibliography is issued in two sections: Section 1 - Abstracts, and Section 2 - Indexes. This issue of the Abstract Section cites 158 patents and applications for patent introduced into the NASA scientific and technical information system during the period of January 1975 through June 1975. Each entry in the Abstract Section consists of a citation, an abstract, and, in most cases, a key illustration selected from the patent or application for patent. This issue of the Index Section contains entries for 2830 patent and application for patent citations covering the period May 1969 through June 1975. The index section contains five indexes -- subject, inventor, source, number and accession number

    Fourth Aircraft Interior Noise Workshop

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    The fourth in a series of NASA/SAE Interior Noise Workshops was held on May 19 and 20, 1992. The theme of the workshop was new technology and applications for aircraft noise with emphasis on source noise prediction; cabin noise prediction; cabin noise control, including active and passive methods; and cabin interior noise procedures. This report is a compilation of the presentations made at the meeting which addressed the above issues

    A review of gear housing dynamics and acoustics literature

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    A review of the available literature on gear housing vibration and noise reduction is presented. Analytical and experimental methodologies used for bearing dynamics, housing vibration and noise, mounts and suspensions, and the overall geared and housing system are discussed. Typical design guidelines as outlined by various investigators are given
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