• Title/Summary/Keyword: Reconnaissance Pod

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Analyses on Aerodynamic and Inertial Loads of an Airborne Pod of High Performance Fighter Jet (고기동 항공기 하부 장착 파드의 공력 및 관성하중 분석 연구)

  • Lee, Jaein;Shin, Jinyoung;Cho, Donghyun;Jung, Hyeongsuk;Choi, Taekyu;Lee, Jonghoon;Kim, Youngho;Kim, Sitae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.1
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    • pp.9-22
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    • 2022
  • A fighter performing a reconnaissance mission is equipped with a pod that drives optical/infrared sensors for acquiring and identifying target information on the lower part of the fuselage. Due to the nature of the reconnaissance mission, the fighter performs high speed evasive maneuvers, and the resulting load should be considered importantly for the development of the pod. This paper concerns a numerical investigation into the inertial and aerodynamic loads of the airborne pod of high performance aircrafts. For the aerodynamic load analysis, the pylon and pod shapes are added to the fighter 3D model, and the commercial software was used for static and dynamic analysis. Considering the practical mission conditions, the common/extreme conditions were established respectively in the static and dynamic situations of pods and the driving torque could be tripled under dynamic conditions. In the analysis of inertia load, a 3-DOF model considering roll and turning maneuvers was derived by the Lagrangian method, and then the numerical integration method was applied to the analysis. As a results, it was conformed that the inertia load was generally induced at a low level compared to the aerodynamic load, but depending on the unbalance mass condition of the pod, the inertia load cannot be negligible.

Experimental Study on the Cooling Characteristics of an Environmental Control System for Avionic Reconnaissance Equipment (항공정찰장비용 환경제어시스템의 냉각특성에 관한 실험적 연구)

  • Kang, Hoon;Park, Hyung-Pil;Lee, Eung-Chan;Kim, Yong-Chan;Chi, Yong-Nam;Choi, Hee-Ju;Byeon, Young-Man;Kim, Young-Jin;Oh, Kwang-Yoon
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.21 no.9
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    • pp.519-526
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    • 2009
  • Environmental control system is adopted to control the thermal load from the avionic equipment in the reconnaissance pod which is mounted under a fighter aircraft, undergoing large and rapid environmental changes with the variations of flight altitude and velocity. In this study, an environmental control system was designed and built by adopting vapor compression cycle using R-124. The cooling performance characteristics of the system were measured varying operating parameters: thermal load in the pod, air mass flow rate through evaporator, condenser inlet air temperature, and air mass flow rate through condenser. The effects of the experimental parameters on the system performance were analyzed based on the experimental results. The problems on the designed system were also analyzed and the solutions were suggested to improve system efficiency and to obtain stable operation.

Experimental Study on the Operating Characteristics of an Environmental Control System for Avionic Equipments (항공장비용 환경제어시스템의 운전특성에 관한 실험적 연구)

  • Park, Hyung-Pil;Kang, Hoon;Chi, Yong-Nam;Choi, Hee-Ju;Byeon, Young-Man;Kim, Young-Jin;Oh, Kwang-Yoon;Kim, Yong-Chan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.9
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    • pp.809-816
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    • 2010
  • An environmental control system is installed to dissipate the thermal load in avionic equipments that are mounted under an aircraft. The operating characteristics of the system change with variations in the control parameters. In this study, an environmental control system was designed and built using R-124 by adopting a vapor compression cycle. The operating characteristics of this system were observed by varying the control parameters, such as refrigerant charging amount, opening of the expansion device, compressor rotation speed, and blower rotation speed. The effect of the control parameters on the environmental control system was analyzed and an optimum control method was identified.

How to Strengthen Convergeance of Special Operations through High-Tech Intertwinement (첨단과학기술의 융복합을 통한 특수작전의 융합성 강화 방안)

  • Sang-Keun Cho;Kang-Il Seo;Min-Seop Jung;Jun-Seong Yoo;Chul-Ki Min;Sang-Hyuk Park
    • The Journal of the Convergence on Culture Technology
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    • v.9 no.2
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    • pp.301-306
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    • 2023
  • Convergeance in the military operations can be attained by simultaneously integrating effects based on sensor, C2, shooter asset in multi-domain and there is no exception to special operations. However, because of challenges from enemy, terrain, geopraphy, and weather, it's not easy to intertwine effects created from ground, sea, air, cyber and electromagnetic spectrum, and space in special operations conducted in deep area. This study presented how to intertwine high-tech such as long-rane reconnaissance·strike drone, cutting-edge sensor, jamming pod, and modular repeater in order to offset aforementioned challenges. Several new high-tech are able to strengthen convergeance of special operations in accordance with the development of the 4th industrial revolution. Therefore, follow-up studies need to be continued making an efforts to search for them.