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      Polybenzimidazole (PBI) Coated CFRP Composite as a Front Bumper Shield for Hypervelocity Impact Resistance in Low Earth Orbit (LEO) Environment

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      https://www.riss.kr/link?id=A105430139

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      다국어 초록 (Multilingual Abstract)

      An object in the Low Earth Orbit (LEO) is affected by many environmental conditions unlike earth’s surface such as, Atomic oxygen (AO), Ultraviolet Radiation (UV), thermal cycling, High Vacuum and Micrometeoroids and Orbital Debris (MMOD) impacts. T...

      An object in the Low Earth Orbit (LEO) is affected by many environmental conditions unlike earth’s surface such as, Atomic oxygen (AO), Ultraviolet Radiation (UV), thermal cycling, High Vacuum and Micrometeoroids and Orbital Debris (MMOD) impacts. The effect of all these parameters have to be carefully considered when designing a space structure, as it could be very critical for a space mission. Polybenzimidazole (PBI) is a high performance thermoplastic polymer that could be a suitable material for space missions because of its excellent resistance to these environmental factors. A thin coating of PBI polymer on the carbon epoxy composite laminate (referred as CFRP) was found to improve the energy absorption capability of the laminate in event of a hypervelocity impact. However, the overall efficiency of the shield also depends on other factors like placement and orientation of the laminates, standoff distances and the number of shielding layers. This paper studies the effectiveness of using a PBI coating on the front bumper in a multi-shock shield design for enhanced hypervelocity impact resistance. A thin PBI coating of 43 micron was observed to improve the shielding efficiency of the CFRP laminate by 22.06% when exposed to LEO environment conditions in a simulation chamber. To study the effectiveness of PBI coating in a hypervelocity impact situation, experiments were conducted on the CFRP and the PBI coated CFRP laminates with projectile velocities between 2.2 to 3.2 km/s. It was observed that the mass loss of the CFRP laminates decreased 7% when coated by a thin layer of PBI. However, the study of mass loss and damage area on a witness plate showed CFRP case to have better shielding efficiency than PBI coated CFRP laminate case. Therefore, it is recommended that PBI coating on the front bumper is not so effective in improving the overall hypervelocity impact resistance of the space structure.

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      참고문헌 (Reference)

      1 Schonberg, W.P., "Studies of Hypervelocity Impact Phenomena as Applied to the Protection of Spacecraft Operating in the MMOD Environment" 204 : 4-42, 2017

      2 ESA, "Space debris Story"

      3 Grossman, E., "Space Environment Effects on Polymers in Low Earth Orbit" 208 : 48-57, 2003

      4 Iqbal, H.M.S., "Processing and Characterization of Space-Durable High-Performance Polymeric Nanocomposite" 25 : 87-95, 2011

      5 Sathish Kumar, S.K., "Polybenzimidazole (PBI) Film Coating for Improved Hypervelocity Impact Energy Absorption for Space Applications" 188 : 72-77, 2018

      6 Kim, Y., "Hypervelocity Impact on Flexible Curable Composites and Pure Fabric Layer Bumpers for Inflatable Space Structures" 176 : 1061-1072, 2017

      7 Schonberg, W.P., "Hypervelocity Impact Response of Aluminum Multi-wall Structures" 25 (25): 363-373, 1991

      8 Eric, L., "Handbook for Designing MMOD Protection" 2009

      9 Kumar, S., "Effect of Atmospheric Pressure Plasma Treatment for Repair of Polymer Matrix Composite for Aerospace Applications" 50 : 1497-1507, 2016

      10 Christiansen, E.L., "Design and Performance Equations for Advanced Meteoroid and debris Shields" 14 (14): 145-156, 1993

      1 Schonberg, W.P., "Studies of Hypervelocity Impact Phenomena as Applied to the Protection of Spacecraft Operating in the MMOD Environment" 204 : 4-42, 2017

      2 ESA, "Space debris Story"

      3 Grossman, E., "Space Environment Effects on Polymers in Low Earth Orbit" 208 : 48-57, 2003

      4 Iqbal, H.M.S., "Processing and Characterization of Space-Durable High-Performance Polymeric Nanocomposite" 25 : 87-95, 2011

      5 Sathish Kumar, S.K., "Polybenzimidazole (PBI) Film Coating for Improved Hypervelocity Impact Energy Absorption for Space Applications" 188 : 72-77, 2018

      6 Kim, Y., "Hypervelocity Impact on Flexible Curable Composites and Pure Fabric Layer Bumpers for Inflatable Space Structures" 176 : 1061-1072, 2017

      7 Schonberg, W.P., "Hypervelocity Impact Response of Aluminum Multi-wall Structures" 25 (25): 363-373, 1991

      8 Eric, L., "Handbook for Designing MMOD Protection" 2009

      9 Kumar, S., "Effect of Atmospheric Pressure Plasma Treatment for Repair of Polymer Matrix Composite for Aerospace Applications" 50 : 1497-1507, 2016

      10 Christiansen, E.L., "Design and Performance Equations for Advanced Meteoroid and debris Shields" 14 (14): 145-156, 1993

      11 Wright, D., "Colliding Satellites: Consequences and Implications" 2009

      12 Baluch, A.H., "Carbon/epoxy Composite Shielding System and Effect of Stuffing Fabric on System Performance" 136 : 182-190, 2016

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      공동연구자 (7)

      유사연구자 (20) 활용도상위20명

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2028 평가예정 재인증평가 신청대상 (재인증)
      2022-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2019-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2016-01-01 평가 등재학술지 선정 (계속평가) KCI등재
      2015-12-01 평가 등재후보로 하락 (기타) KCI등재후보
      2013-02-01 학술지명변경 한글명 : 한국복합재료학회지 -> Composites Research
      외국어명 : JOURNAL OF THE KOREAN SOCIETY FOR COMPOSITE MATERIALS -> Composites Research
      KCI등재
      2011-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2006-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보학술지 유지 (등재후보1차) KCI등재후보
      2003-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.34 0.34 0.33
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.28 0.25 0.439 0.03
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