• 제목/요약/키워드: stealth

검색결과 172건 처리시간 0.027초

Tests on Ventilation Control of PRAIRIE for Improving Acoustic Stealth Performance (음향스텔스 성능 향상을 위한 PRAIRIE 공기 분사량 제어 실험)

  • Lee, Heechang;Moon, Youngsun;Kang, Seunghee
    • Journal of the Korea Institute of Military Science and Technology
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    • 제23권6호
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    • pp.602-608
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    • 2020
  • PRAIRIE(Propeller Air Induced Emission) system is a kind of underwater radiated noise suppression systems to reduce the probability of the identification or classification of our warship's acoustic signature by an enemy ship. It is effective in case of strong cavitation events. This is because air bubbles emitted from the PRAIRIE system mitigate drastic collapses of the cavity bubbles that can generate an intense shock wave. However, when the PRAIRIE system is operated in a non or weak cavitation condition, it might increase the total level of underwater radiated noise and induce the acoustic signatures. Therefore, this paper presents the trial results on ventilation control of PRAIRIE to find a more efficient operation depend on the cavitation condition. Then, we show a variation of the amplitude modulation characteristics according to ventilation control.

Flow Visualization Study on Vortices over a Stealth UCAV Configuration (스텔스 무인전투기 형상의 와류 거동에 대한 흐름가시화 연구)

  • Kang, Seung-Hee;Lee, Do-Kwan;Hyun, Jae-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제35권6호
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    • pp.467-473
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    • 2007
  • Flow visualization study to qualitatively define the flow field over a stealth UCAV(Uninhabited Combat Air Vehicle) configuration in a water tunnel has been conducted to clarify the basic aerodynamic performance. The test was performed at freestream velocity of 12.7 cm/sec which was corresponding to a Reynolds number of $1.4{\times}10^4$ based on mean aerodynamic chord. The development and breakdown of vortices illuminated by using dye were compared to the previous force and moment data. It was shown that the effect of the vortices generated by the main-body and junction are dominant in the low angle-of-attack region. However, in the high angle-of-attack region, the vortex generated by the fore-body mainly influenced the aerodynamic performance of the model.

A Study on Measurement Techniques of EM Wave Absorbing Ability of a RAM for RF Stealth (RF 스텔스용 RAM의 전파흡수능 측정기법에 관한 연구)

  • Choi, Chang-Mook;Lim, Bong-Taeck;Ko, Kwang-Soob
    • Journal of the Korea Institute of Information and Communication Engineering
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    • 제14권6호
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    • pp.1331-1337
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    • 2010
  • In this paper, measurement techniques of absorbing ability for a RAM were studied for RCS Reduction needed for materializing ADD's RF stealth. As for the measurement techniques of absorbing ability, the theories of the free space method, similar to real radar system, and transmission line method, suitable for lab scale, were established. And we made real RAM samples, measured absorbing ability according to each, and compared the results. After comparison, electromagnetic(EM) wave absorbing ability was measured to be somewhat superior in free space method and overall uniform pattern was observed. Therefore, by applying measurement techniques by stage and by frequency we could develop RAM in a more efficient way.

Analysis of Radar Cross Section of the Tank and Its Application at Millimeter Wave W-Band (밀리미터파 W-대역에서 전차의 레이다 단면적 해석 및 응용)

  • Shin, Hokeun;Song, Sung Chan;Kim, Jihyung;Park, Yong Bae
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • 제28권9호
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    • pp.756-759
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    • 2017
  • In this paper, the radar cross section of a tank is analyzed at millimeter wave W-band. We calculate the radar cross section of the tank using the program based on PO and PTD and the computed results are compared with those of commercial simulator to check the accuracy of computations. The radar cross section is calculated in terms of the incident angle, polarization, and tank with or without cannon. The radar cross section can be reduced by changing the shape of the turret that can be applied to stealth tanks.

The Magnetic Treatment Method for Low-Observable Naval Vessel (해군함정의 영구자기장 감소를 위한 탈자기법)

  • Kim, Hwiseok;Lim, Seonho;Doh, Jaewon
    • Journal of the Korean Magnetics Society
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    • 제24권4호
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    • pp.128-133
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    • 2014
  • The control and reduction of the magnetization of naval vessel is important technologies for safety against torpedo and sea mine installed magnetic sensors. In general, we used to conduct as a magnetic treatment for permanent magnetization reduction and to compensate induced magnetization using on-board-degaussing system for the naval vessel's magnetic stealth. Navies have operated magnetic treatment facility in order to protect from sea mines. LIGNex1 Corp. has developed the magnetic treatment facility for the korea navy.

A Study on Dipole Modeling Method for Ship's Magnetic Anomaly using Singular Value Decomposition Technique (특이치 분해 방법에 의한 함정 자기원 다이폴 모델링 방안 연구)

  • Yang, Chang-Seob;Chung, Hyun-Ju
    • Journal of the Korean Magnetics Society
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    • 제17권6호
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    • pp.259-264
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    • 2007
  • This paper describes the mathematical modeling method for the static magnetic field signature generated by a magnetic scale model. we proposed the equivalent dipole modeling method utilizing a singular value decomposition technique from magnetic field signatures by magnetic sensors are located special depths below the scale model. The proposed dipole modeling method was successfully verified through comparisons with the real measured values in our non-magnetic laboratory. Using the proposed method, it is possible to predict and analyze static magnetic field distributions at any difference depths generated from the real ships as well as a scale model ship.

An Estimation of RCS through Configuring Element Analysis (형상요소분석을 통한 레이더단면적의 추정)

  • Kwon, T.J.;Shin, Bo-Hyun
    • Journal of the Korea Institute of Military Science and Technology
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    • 제15권4호
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    • pp.417-423
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    • 2012
  • Radar Cross Section(RCS) is a measure of how detectable an object is with a radar. A larger RCS indicates that an object is more easily detected. Informally, the RCS of an object is the cross-sectional area of a perfectly reflecting sphere that would produce the same amount of reflection strength as the object in question would. In order to estimate RCS of aircraft weapons the external surface is modeled as a collection of simple shape elements. And the overall RCS is estimated as a vector sum of configuring elements' cross-sections which are well known given by analytic formulae. A RCS estimation code is developed for a typical shape of Air-To-Surface bombs and missiles. Size of weapons and location of fins are implemented in the code in addition to the presence of canards. The ability to predict radar return from flying vehicles becomes a critical technology issue in the development of stealth configurations. This simplified method of RCS estimation is known to be fast and accurate enough in an optical region of high frequency incident radio wave.

Design of Transparent Electromagnetic Absorbing Structure using Metal Grid Mesh Printing (Metal Grid Mesh 인쇄를 이용한 투명 전파 흡수구조 설계)

  • Yoon, Sun-Hong;Lee, Jun-Sang;Lee, In-Gon;Hong, Ic-Pyo
    • Journal of the Korea Institute of Military Science and Technology
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    • 제19권3호
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    • pp.294-301
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    • 2016
  • In this paper, we designed the transparent circuit analog radar absorbing structure using printed metal grid mesh for enhanced optical transmittance. To obtain wideband electromagnetic absorption and enhanced optical transparency at X-band, we proposed the resistive FSS(Frequency Selective Surface) using printed metal mesh pattern on transparent glass with PEC(Perfect Electric Conductor) plane using ITO(Indium Thin Oxide) coating. We then fabricated the proposed structure to verify the simulation results obtained from commercial EM simulator. The comparisons between the simulation and measured results show good agreements. The results also show that the proposed radar absorbing structure can provide wideband reflection as well as better optical transparency. We can apply this proposed structure to the canopy of stealth aircraft and other stealth and security applications for visible transparency.

IR Characteristics of an Aircraft in Different Atmospheric/Background Conditions (대기/배경에 따른 계절별 항공기 적외선 방사 특성)

  • Kim, Taehwan;Song, Jiwoon;Cha, Jong Hyun;Bae, Ji-Yeul;Jung, Daeyoon;Cho, Hyung Hee
    • Journal of the Korea Institute of Military Science and Technology
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    • 제17권4호
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    • pp.456-462
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    • 2014
  • Infrared(IR) guided heat-seeking missiles uses IR emissions from aircraft to detect and track a target. Due to passive characteristic of the IR guidance, early detection of the missile is difficult and it is significant threat to aircraft survivability. Therefore, IR signature prediction of the aircraft is an important aspect of the stealth technology. In this study, we simulated IR signature of the aircraft in real atmospheric conditions. Aircraft surface temperature distribution was calculated by using RadthermIR code. Based on temperature distribution, IR radiance and BRDF(Bidirectional Reflectance Distribution Function) image were simulated for different weather(seasonal) and background(sky/soil) conditions. The IR contrast tendencies are not aligned with surface temperature or magnitude of target IR radiance. Therefore, it is essential to simulate IR signature with various conditions and background to acquire reliable database.

Thermal Radiative Properties of Multilayer Graphene/Glass Structure (다층 그래핀/유리 구조체의 적외선 열복사 특성 연구)

  • Park, Kyung-Ah;Lim, Mikyung;Jung, Hyun-June;Kim, Jae-Hyun
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • 제34권1호
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    • pp.27-32
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    • 2021
  • In this study, we fabricated multilayer graphene on a glass substrate by stacking the monolayer graphene synthesized via chemical vapor deposition. The electrical sheet resistance and optical transmittance were evaluated to confirm the quality of the stacked multilayer graphene. Using the fabricated multilayer graphene/glass structure, we characterized its thermal radiative property in terms of the integrated emissivity. The integrated emissivity of the multilayer graphene/glass structure was tuned from 0.91 to 0.72 when the number of graphene layers was changed from 1 to 12. We also demonstrated that the emissivity tunability provided a way to control the apparent temperature of an object that can be used in infrared stealth applications.