• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.193-196
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• 2007

The motor case for the KSLV-I KM is the first satellite launch vehicle ever to be developed by Korea to deliver the 100 kg class satellite into Earth's low orbit. This SLV is made of two stages, and the 2nd stage is made of solid rocket motor. The motor case of the KM is made of all composite materials except for the interface structures. Manufacturing process for the motor case such as insulation, filament winding for the motor case, fabrications for the interface structures will be discussed in this paper.

• Journal of the Korean Society of Propulsion Engineers
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• v.2 no.3
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• pp.107-115
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• 1998

This paper deals with the study on injection with EPDM(Ethylene propylene dien ter polymer) the gap which narrow, long, and tubular between an ablative composite tube and a steel motor case. Small size motor assembly was designed and manufactured for man-portable air defense propulsion system. Motor assembly is consisted with steel tube, ablative composite tube and insulation rubber. Ablative composite tube was made of carbon/phenolic prepreg by rolling process and insulation rubber was made of EPDM by TPM(Trans-power molding) process. To select the insulation rubber material, we tested ablative insulation property and degradation property at first and we tested fluidity, adhesive property and hardness of EPDM rubber. Finally we designed TPM process to manufacture motor case assembly and the motor case assembly was examined by non-destructive test(X-ray).

• Journal of the Korean Society for Nondestructive Testing
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• v.21 no.3
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• pp.313-318
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• 2001

To establish nondestructive test method for aerospace composite materials, various composite specimens were tested and analyzed using acoutic emission. The hit rate of acoustic emission closely was rotated with crack initiation and propagation. This report also presents defection capability of crack initiation pressure, initial crack active location, and crack propagation using acoustic emission.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.2
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• pp.200-205
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• 2010

Heat-resistance of W/$Y_2O_3$ as throat insert material was evaluated to develop rocket motor keeping thrust uniformly under condition of high-temperature, high-pressure and long-burn time. Test was conducted with varying burn time, and test results were compared with CIT. Test showed that ablation rate was decreased according as burn time was increased, and that ablation rate of W/$Y_2O_3$ was about 55 % of CIT. Macro/micro structures of throat insert did not show a peculiar phenomenon by increased burn time. In addition, the vacuum heat treatment is effective for the prevention of crack in throat insert.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.4
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• pp.47-53
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• 2006

In this paper, the thermal insulator structure of a real rocket which is fabricated in a way that laminated composite rings are connected in series is analyzed using 3-dimensional axisymmetric finite element models. Simulation of cowl zone using a real operating conditions provides that the stress distribution in the laminated composite ring is largely influenced by ply-angles, axial dimensions, and boundary conditions. Notably the plylift that is the precursor to the wedge-out occurs in the ring-to-ring bonding region. It is hypothesized that after the plylift the wedge is dropped out due to the shear stresses in the ply-angle direction and axial compressive stresses.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2009.10a
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• pp.207-207
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• 2009

요업 소성로에서 내화재로 흡수된 에너지는 피가열물에 방사열로 작용하며, 이때 내화물의 방사율이 높을수록로내의 온도를 상승시켜 소비되는 연료가 절감된다. 따라서 내열성과 방사율이 높은 세라믹 내열도료를 개발하여 구성물의 결정 구조, 열적특성, 적외선 방사량 및 에너지 절감실험에 대한 데이터를 분석한 결과 높은 내열성과 적외선 방사량 증가에 따른 에너지 절감에 효과가 있음을 알 수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.04a
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• pp.18-18
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• 1999

추진제의 비추력 및 밀도 등을 효과적으로 증진시키기 위해 알루미늄 분말의 함량을 높인 고 알루미늄 추진제가 로켓모터에 널리 사용되고 있다. 추진제 내 알루미늄 성분은 연소과정의 이상유동으로 인하여 로켓의 성능 및 내열설계에 많은 영향을 미칠 수 있다. 즉, 산화알루미늄 입자가 노즐 벽면에 달라붙어 추력의 손실을 가져오기도 하고 노즐 입구에 침적되어 내열재의 삭마가 과다해져 최악의 경우 모터의 파손을 일으켜 임무수행에 실패를 초래할 수도 있다.

• Journal of the KSME
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• v.26 no.4
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• pp.284-289
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• 1986

이들 기기, 장치는 대부분 철강재가 그 근간을 이루고 있지만, 특히 고온부를 형성하는 부재는 내열용 철강과 합금이다. 강을 모재로 하고 고온에서의 강도유지를 위하여 유용한 소랴의 Cr, Mo 등을 합금시킨 저합금내열강이 1차적으로 사용되어 왔으나 사용조건이 고도화 되면서 이들 합금성분 량이 늘어나 주로 Cr 성분을 증가시킨 고 Cr 페라이트계, 그리고 Ni 성분을 다량으로 첨가한 오스테나이트계 내열강이 제 2차, 제 3차대상이 되어 연구 발전되어 왔다. 그 사용한계는 사용 가스등 환경의 영향과 고온의 크리이프나 피로, 파괴에 대한 저항성등에 크게 좌우되지만, 대개 2.25Cr-1Mo 강의 저합금강에서 $550^{\circ}C$, 9~12% Cr인 페라이트계 내열강에서 $^650{\circ}C$ 까지가 한도이며 그 이상온도에서는 오스테나이트계 내열강이 고려의 대상이 되고 있는 것 같다. 이들 고온부에 사용되는 철강 재료를 중심으로 최근의 동향을 주로 금속학적 입장에서 살펴보기로 한다.

• Journal of Advanced Marine Engineering and Technology
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• v.7 no.2
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• pp.36-49
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• 1983

최근 높은 경제성과 용접성의 우수성에 의한 마찰 용접의 응용에 있어서 내열.내식 재료가 개스터어빈, 기관, 핵 발전기등의 기계 부품 생산 공업에 널리 이용되고 있다. 따라서 이종내열 합금강의 마찰 용접된 부품을 이용함에 있어서 내식.내마모 및 용접성 뿐만 아니라 고온 피로 강도와 크리이프 강도 등의 복합 특성에 관한 연구가 요구되고 있다. 본 연구에서는 마르텐사이트계 실크롬 내열강과 오오스테나이트계 닉켈크롬 스테인레스강의 이종 내식.내열 합금강의 최적 용접조건하에서 마찰 용접된 후의 시효 열처리가 용접재의 700 .deg.C 고온 회전 굽힘 피로강도 특성에 미치는 영향에 관하여 실험과 강도해석에 의해 조사되었고 용접후의 용체화 처리와 시효 열처리법에 의한 내열강 마찰 용접강도 개선법을 개발코저한 것이다.

• Applied Chemistry for Engineering
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• v.29 no.2
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• pp.201-208
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• 2018

The ortho- and iso- type unsaturated polyester resins were synthesized and used as a polymer binder of the polymer mortar composite. Styrene monomer and acrylonitrile were used as a diluent for the unsaturated polyester resin. Methyl ethyl ketone peroxide (MEKPO) and cobalt octoate (CoOc) were used as a curing agent and an accelerator, respectively. Four kinds of unsaturated polyester resins were prepared according to types of the resin and diluent, and used as a polymer binder in the preparation of the specimen. A total of 16 polymer mortar specimens were prepared according to the added amount of the polymer binder and subjected to a hot water resistance test, followed by compressive and flexural strength tests, and pore and SEM analyses. As a result, it was found that the strength of the specimen using the iso-type unsaturated polyester resin as the polymer binder was better than that of using the ortho-type unsaturated polyester resin. The total pore volume and diameter measured after the hot water resistance test were reduced compared to the values before the test. In the micrographs observed before the hot water resistance test, the polymer binder, filler and fine aggregate were firmly combined to the co-matrix, but the polymer binder was mostly decomposed in the micrographs observed after the test.