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- W1987657258 abstract "우주 구조물을 위협하는 여러 요소들 중 MMOD(MicroMeteoroid and Orbital Debris)는 약 8~70km/s의 속도로 우주 구조물과 충돌하여 큰 피해를 주고 있다. 이러한 피해로부터 우주 구조물을 보호하기 위해서 현재 다양한 위플 쉴드가 연구, 적용되고 있다. 위플 쉴드에는 알루미늄이 주로 사용되고 있지만, 복합재료의 시용도 증가하고 있어 본 연구에서는 알루미늄과 복합 재료의 초고속 충돌 특성을 유한 요소 해석을 통해 비교하였다. 충격체는 직경 5.5mm인 알루미늄 2017-T4의 구를 사용하였고, 알루미늄 평판은 6061-T6, CFRP 평판은 T300/5208을 사용하였다. 충격체의 초기 충돌 속도는 1km/s이다. 충돌 후 충격체의 운동에너지는 알루미늄 평판의 경우 약 64J 감소하였고, CFRP 평판의 경우 약 63J 감소하였다. 비슷한 충돌 에너지 흡수 정도를 보이고 있지만, 밀도를 비교해 보았을 때 CFRP가 약 1.7배 가볍기 때문에 방탄 특성이 더 좋다고 할 수 있다. Among the factors that threaten spacecraft, Micrometeoroid and Orbital Space Debris(MMOD) cause damage to spacecraft and impact velocity is about 8~70km/s. Nowadays, various Whipple Shield are studied and applied to protect spacecraft. As the materials used to Shielding System, aluminum is usually used but composite is also used increasingly. So this study compared characteristics of hypervelocity impact of Aluminum and composites through finite element analysis. The Projectile was a spherical shape using Aluminum 2017-T4, and aluminum plate was using Aluminum 6061-T6, CFRP plate was using T300/5208. Initial impact velocity of projectile was 1km/s. As a result, kinematic energy of projectile decreased to about 64J and about 63J for aluminum plate and CFRP plate, respectively after impact. Although both results is almost same about the absorption of impact energy, you can think the CFRP has good ballistic characteristic, because CFRP is lighter about 1.7 times compared with density of aluminum." @default.
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- W1987657258 date "2010-12-31" @default.
- W1987657258 modified "2023-09-25" @default.
- W1987657258 title "Hypervelocity Impact Analysis Of Composite Plate For Space Shielding System" @default.
- W1987657258 cites W1991020008 @default.
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- W1987657258 doi "https://doi.org/10.7234/kscm.2010.23.6.014" @default.
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