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미사일 발사체 포드의 진동 및 충격 안전성 검증에 관한 연구

Vibration and Shock Safety Verification for Missile Launcher Pod

  • 투고 : 2014.12.29
  • 심사 : 2015.05.23
  • 발행 : 2015.06.15

초록

The launcher pod for missiles capable of carrying a range of different warheads has been designed to be mounted on the tracked vehicle of the hybrid weapon system (HWS). In the development of this launcher pod, its structure was designed to be resilient to damage caused by shock and vibration, as well as preventing assembly errors due to the spring-back of the main composite cover and interfacing parts. This study investigated the design of the newly developed launcher pod, with its hybrid composite-metal structure, through simulation and experiment. Both simulation and actual experiments showed that the structure of the launcher is resilient to vibration and shock. The launcher pod was also subjected to vibration and shock tests to verify its performance.

키워드

참고문헌

  1. Kim, J. H. Jeon, K. H., 2011, Design of Isolators for Missile-pod System of a Tracked Vehicle, Proc. Korea Institute of Military Science and Technology Conference, 2038-2041.
  2. Isolator Selection, n.d. viewed August 2013,
  3. NX Nastran, 2011, NX Response Simulation Lecture Notes SIEMENS Inc.
  4. Irvine, T., 2013, Effective Modal Mass & Modal Participation Factors.
  5. Wijker, J., 2009, Random Vibrations in Spacecraft Structures Design, Springer Dordrecht Heidelberg London, New York.
  6. Steinberg, D. S., 2000, Vibration Analysis for Electronic Equipment, John wiley & Sons Inc, Canada.
  7. Data Physics, 2002, Making Measurements with SignalCalc ACE, Data Physics Corp.
  8. MIL, 1989, Test Method Standard for Environmental Engineering Considerations and Laboratory Tests. MIL-STD-810F, Department of Defence.
  9. Kim, M D., Hong, S. W., 2014, A Study of the Vibration and Shock Verification for Missile POD, Proc. of KSME, 2303-2306.

피인용 문헌

  1. Study of the Vibration and Shock Isolation for HEV Battery Pack vol.33, pp.10, 2016, https://doi.org/10.7736/KSPE.2016.33.10.813