• Title/Summary/Keyword: 초고주파 탐색기

Search Result 2, Processing Time 0.014 seconds

A Study on the Thermal Design for A Signal Processor in the Micro-Wave Seeker (초고주파 탐색기 신호처리부의 방열설계에 관한 연구)

  • Lee, Won-Hee;Yu, Young-Joon;Kim, Ho-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.39 no.1
    • /
    • pp.76-83
    • /
    • 2011
  • This paper focuses on the thermal design of a signal processor in Micro-Wave Seeker. High temperature environment and ESS(Environmental Stress Screening) test condition should be considered in designing a signal processor. First, we performed the thermal analysis to know conditions under which a signal processor is thermally reliable. As a result of thermal analysis, we found that adopting heat transfer block to the thermally fragile components is most efficient, because the heat transfer block can control the thermal loads of the individual components. Next, we verified this solution by numerical simulation and experiment and concluded that thermal reliability of a signal processor can be achieved. Maximum temperature difference between numerical simulation and experiment is about $2^{\circ}C$.

Estimation of Ground Clutter Reflectivity based on the CFT(Captive Flight Test) (항공기 탑재 시험을 통한 지상 클러터 반사계수 추정)

  • Son, Chang-Hee
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.9 no.2 s.25
    • /
    • pp.87-95
    • /
    • 2006
  • The performance of a microwave missile seeker and radar operating in an air-to-air look-down mode is strongly influenced by the presence of ground clutter In order to correctly account for the effects of ground clutter, it is required to develop a model capable of representing clutter characteristics as a function of range and/or frequency. In this paper, a program to estimate the clutter reflectivity for various ground conditions is developed, using the actually measured data and the data available from open literatures. In addition, clutter characteristics measured for various ground conditions such as sea, agricultural area, urban city and industrial area through the captive flight tests are presented.