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파이로추력기의 점화시간차 영향

Effect of Ignition Delay Time Gap on the Linked Pyrotechnic Thrusters

  • 김기언 (국방과학연구소 대함유도무기체계개발단) ;
  • 전인수 (국방과학연구소 대함유도무기체계개발단) ;
  • 안성우 (국방과학연구소 대함유도무기체계개발단)
  • 투고 : 2010.11.26
  • 심사 : 2011.01.20
  • 발행 : 2011.02.05

초록

The effect of the ignition delay time gap is newly studied. The operational characteristics of the linked two pyrotechnic thrusters are affected by the time gap. Although two thrusters are simultaneously ignited, the time at which the pressure starts to rise in each thruster may not be synchronized. The characteristic of the system with the time gap is compared with that of the fully synchronized system without any time gap. Depending upon the magnitude of the time gap, the pressure-time profile and the ballistic performance are different. When two pyrotechnic thrusters have a time gap, the peak pressure of one thruster(in which the pressure is built up earlier) is increased and the other is decreased. As the time gap is increased, the peak pressure is converged into the maximum pressure. This maximum pressure can be obtained when only one thruster is activated. Because the maximum pressure is bounded, it is predicted that there isn't any catastrophic failures in the considered system. When the time gap is relatively small, the impulse of the combined force acting on the moving body is almost maintained. But the ballistic performance of the system with a large time gap should be carefully estimated because the reduction of the ballistic performance should not be easily neglected.

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참고문헌

  1. Toewee, G., Tirmizi, A., Blachowski, T. J., and Culhane, D. A., "U.S. Navy and the CAP/PAD Joint Program Office Electronic Time Delay Cartridge Development Program", AIAA 2008-5078, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 21-23 July 2008.
  2. 오석진, 이도형, 김상화, 김기언, "가스발생기를 이용한 분리 메카니즘 성능예측 기법", 한국추진공학회 2008년도 추계학술대회 논문집, pp. 1-4.
  3. Lee, H. S., "Unsteady Gasdynamics Effects in Pyrotechnic Actuators", Journal of Spacecraft and Rockets, Vol. 41, No. 5, pp. 877-886, September- October 2004. https://doi.org/10.2514/1.2594
  4. Lee, H. S., "Ignition Delay Investigation in a Pyrotechnic Cartride with Loosely-Packed Propellant Grains", AIAA 2009-5191, 45th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit, 2-5 August 2009, Denver, Colorado