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"구조"

Regulars

Lightweight Design of a Guided Missile Control Fin Using Metal Additive Manufacturing-based Lattice Structures
Cho Bin Lee, Ye Sung Jeon, Jae Min Park, Jin Ho Jeong, Kyu Tae Shin, Hyeon Jin Son, Dong Wan Lee, Ji Min Park, Hyun Chan Kim, Soon Jo Kwon
J. Korean Soc. Precis. Eng. 2026;43(7):767-778.
Published online July 1, 2026
DOI: https://doi.org/10.7736/JKSPE.026.00026
The control fin is a key component in a guided missile's propulsion system, stabilizing the missile's attitude and maintaining its flight trajectory under high-speed conditions. Such components demand high mechanical strength and thermal stability. However, traditional control fin designs have primarily focused on external geometry, overlooking opportunities to enhance performance through internal structural design.To address this limitation, this study proposes a design approach that integrates lattice structures within the control fin using metal additive manufacturing. A body-centered cubic (BCC) lattice was selected, with strut diameter and unit cell aspect ratio defined as the primary design variables. Finite element analysis in Abaqus was used to evaluate structural behavior, analyzing stress and displacement distributions based on variations in these lattice parameters. Manufacturability and lightweight characteristics were also assessed. Results indicate that increasing the strut diameter improves structural stability, with stress predominantly concentrated near lattice joints. Building on these findings, a non-uniform lattice design, derived from the uniform lattice analysis, was applied, demonstrating improved stress distribution and overall structural performance. This approach shows that lattice-based internal structures, enabled by metal additive manufacturing, can significantly enhance the structural performance of guided missile control fins while achieving substantial weight reduction.
  • 1,332 View
  • 18 Download
Structural Analysis Study for Performance Enhancement of 3D-printed CANSAT Structures
Youngmo Seong, Eungdo Kim, Hyochang Lee, Jinsung Rho, Changbeom Choi
J. Korean Soc. Precis. Eng. 2026;43(6):653-660.
Published online June 1, 2026
DOI: https://doi.org/10.7736/JKSPE.025.131
The nano satellite industry has transitioned to low-cost development, driven by private companies and research organizations in the NewSpace era. Can-Satellite offers a budget-friendly alternative to traditional cube satellite manufacturing and testing. This study focuses on enhancing the reliability of small satellite designs by analyzing the vibration stability of PLA plates, the primary structure of a Can-Satellite, produced through Fused Filament Fabrication (FFF) 3D printing. Quasi-static, modal, and random vibration analyses were conducted using Finite Element Analysis (FEA) with ANSYS to evaluate stacking directions along the x, y, and z axes and optimize structural stability. The findings indicate that the y-axis laminated structure exhibits superior vibration endurance, effectively reducing issues during launch. This research contributes to improving the reliability of Can-Satellites and enhances manufacturing efficiency for cube and micro-satellite projects. Additionally, it supports the advancement of educational satellites and domestic small satellite technology.
  • 656 View
  • 19 Download
Advanced Thermal-structural Coupling Analysis of Semiconductor Probe Card based on Ansys APDL and Point Cloud Meshing
Seong Hoon Kim, Min Seong Oh, Ji Eun Kim, Kyeong Hoon Lee, Seok Moo Hong
J. Korean Soc. Precis. Eng. 2026;43(4):378-384.
Published online April 1, 2026
DOI: https://doi.org/10.7736/JKSPE.025.135
The semiconductor industry is experiencing significant growth in production scale and investment, driven by rising demand for generative AI, high-performance computing (HPC), high-bandwidth memory (HBM), and high-performance/high-density chips. As a result, precision inspection and yield management at the wafer stage have become critical challenges. Probe cards, essential for verifying a chip's electrical performance, play a vital role in yield management. However, during repetitive inspection processes, probe cards absorb heat from the underlying chuck, leading to probe tip-pad alignment errors that degrade contact reliability and measurement accuracy. This situation necessitates a quantitative evaluation system based on thermo-structural coupled analysis. Additionally, the modeling process for multiple interposers and interposer housings, along with the preprocessing of contact conditions, adds complexity due to the increasing number of contact surfaces. This complexity can result in convergence issues and reduced accuracy. To address these challenges, this study employs Ansys Parametric Design Language (APDL) to enhance interposer and housing modeling, as well as contact problem resolution. It introduces a novel meshing method that positions nodes at target coordinates using point clouds, providing an effective analysis approach applicable to large, high-density probe cards and thermo-structural problems involving numerous contacts.
  • 304 View
  • 19 Download

Special

Cross-sectional Design Optimization and Structural Safety Evaluation of PFRP Photovoltaic Support Structure
Min Seo Jeong, Yong Jae Lee, Gyu Min Kim, Ji Yun Jang, San Kim
J. Korean Soc. Precis. Eng. 2026;43(3):257-266.
Published online March 1, 2026
DOI: https://doi.org/10.7736/JKSPE.025.00037
This study examines a 2kW photovoltaic (PV) support structure, highlighting the vulnerability of conventional metal frames to corrosion and strength degradation in harsh environmental conditions. To overcome these challenges, we propose using pultruded fiber-reinforced polymer (PFRP) members as an alternative structural material. An optimal design framework is established to identify efficient PFRP cross-sections. The study aims to determine lightweight cross-sectional dimensions for box sections (columns and girders) and C-sections (purlins) while maintaining structural safety. We evaluate structural performance using the allowable stress design (ASD) method, incorporating safety factors recommended by the American Association of State Highway and Transportation Officials (AASHTO). Finite element analysis (FEA) assesses critical design constraints, including buckling, material failure, and serviceability deflection limits. From the feasible designs, we select the lightest cross-sectional configuration that meets all safety requirements. The results demonstrate that PFRP members can significantly reduce weight while ensuring structural safety, thus validating their potential as an alternative to conventional metal photovoltaic support structures.
  • 489 View
  • 18 Download

Regulars

Structural Design and Analysis of a Quadcopter Type CanSat for Diverse Launch Conditions
Yongseon Lee, Hyeongyu Lim, Hyeonchang Yang, Changbeom Choi, Jinsung Rho
J. Korean Soc. Precis. Eng. 2026;43(1):29-36.
Published online January 1, 2026
DOI: https://doi.org/10.7736/JKSPE.025.043
This study evaluates the structural design and safety of the CanSat in launch environments. The CanSat serves as an educational replica satellite, allowing users to experience the design and operation of small satellites. To ensure stable operation during launch, the structural analysis and design must consider external forces, including vibration and acceleration loads. We determined the material properties for the structure and conducted modal and random vibration analyses, comparing the results with launch environment data from NASA, ECSS, Falcon 9, and Soyuz-2. Additionally, we performed an acceleration load analysis using actual data from CanSat launches during competitions. The modal analysis indicated that the first natural frequency was 65.34 Hz, which exceeds the required threshold. The random vibration and acceleration load analyses further confirmed the structural safety of the design. While the data from NASA and ECSS were conservatively set, reflecting higher vibration intensities, the Falcon 9 and Soyuz-2 launch vehicles provided relatively lower vibration environments due to differences in their designs. Overall, the results demonstrate that the CanSat's structural integrity is maintained under the conditions analyzed for Falcon 9 and Soyuz-2.
  • 1,309 View
  • 38 Download
Lightweight Design and Dynamic Verification of Multi-layer Sarrus Deployable Structures for Rotor-sail under Centrifugal Loading
Chan Kim, Sun-Pill Jung, JangGil Kim, Kyu-Jin Cho
J. Korean Soc. Precis. Eng. 2025;42(12):1099-1106.
Published online December 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.109
This study presents a vertically deployable rotor-sail structure utilizing multi-layer Sarrus linkages. The structure fully extends during sailing to maximize Magnus lift and compresses to less than half its length for docking. An analytical beam model integrates link thickness, mid part spacing, and centrifugal loading to predict deflection and mass. Parametric comparisons of two-layer, six-layer, and twelve-layer configurations reveal that the twelve-layer design reduces structural mass by 90% while meeting an L/1000 deflection limit. Dynamic simulations using RecurDyn confirm that mid part segmentation decreases damping time and reduces peak stress, thus enhancing deployability and mechanical reliability. The findings offer quantitative design guidance for high-speed rotating deployable structures.
  • 344 View
  • 17 Download
Analysis of Convective Heat Transfer Coefficient of Double-wall Gyroid TPMS under Constant Surface Temperature Conditions
Sohyun Park, Jihyun Sung, Dahye Kim, Kunwoo Kim
J. Korean Soc. Precis. Eng. 2025;42(12):1071-1077.
Published online December 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.026
In this study, we comparatively analyzed the convective heat transfer performance of single-wall and double-wall Gyroid TPMS (Triply Periodic Minimal Surface) structures. Using computational fluid dynamics (CFD), we evaluated the average convective heat transfer coefficients under constant surface temperature conditions for both constant velocity and constant pressure flow. Although both structures maintained the same fluid volume, the double-wall configuration increased the surface area by approximately 1.8 to 1.9 times, resulting in enhanced heat transfer performance. Under constant velocity conditions, the double-wall structure exhibited an average convective heat transfer coefficient that was 1.3 to 1.4 times higher than that of the single-wall structure. Under constant pressure conditions, we observed an increase of 1.06 to 1.1 times. Despite the double-wall structure leading to greater pressure losses due to increased shear stress from the formation of microchannels, it still maintained improved heat transfer performance even with reduced mass flow rates under constant pressure conditions. These findings provide fundamental data for designing TPMS-based cooling systems and optimizing additive manufacturing processes.
  • 343 View
  • 19 Download

REGULARs

A Study on the Performance Enhancement of Solid Oxide Fuel Cells by Controlling the Infiltration Molar Concentration of PNO
Miju Ku, Jisung Yoon, Young-Beom Kim
J. Korean Soc. Precis. Eng. 2025;42(11):943-947.
Published online November 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.076

In this study, we employed an infiltration technique to create a nanostructured functional layer, enhancing the electrochemically active area in solid oxide fuel cells (SOFCs). We infiltrated Pr2NiO4+δ (PNO) into a porous GDC electrolyte, resulting in a nanostructured catalytic layer. We characterized its microstructure and cross-sectional morphology using field-emission scanning electron microscopy (FE-SEM). The electrochemical performance was assessed at 750°C with a NiO-YSZ/YSZ/GDC half-cell configuration. The reference cell without PNO infiltration achieved a maximum power density of 2.07 W/cm2, while the cell with 0.05 M PNO infiltration reached an improved value of 2.55 W/cm2. These results demonstrate that by optimizing the infiltration concentration of PNO, we can fabricate a high-performance nanostructured functional layer without adding extra thickness, confirming infiltration as an effective strategy for enhancing SOFC performance.

  • 343 View
  • 8 Download
Tape-casting Process Electrochemical Characteristic Test for Fabrication of LST-GDC for Anode Supported SOFCs
Min Ji Kim, Chunghyun Kim, Young-Beom Kim
J. Korean Soc. Precis. Eng. 2025;42(11):937-942.
Published online November 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.073

In this study, we developed a composite anode support composed of La-doped SrTiO3 (LST) and Gd-doped CeO2 (GDC) using a tape casting process for solid oxide fuel cells (SOFCs). By adjusting the pore former content in the slurry, we constructed a bilayered structure consisting of a porous anode support layer (ASL) and a dense anode functional layer (AFL) with the same material composition. The number of tape-cast sheets was controlled to tailor the overall thickness, and lamination followed by co-sintering at 1250oC resulted in a mechanically robust bilayer. We characterized the microstructural evolution concerning sintering temperature and pore former content using SEM, while XRD confirmed the phase stability of LST and GDC. The measured electrical conductivity at 750oC ensured sufficient electron transport. To enhance interfacial adhesion and suppress secondary phase formation, we introduced a GDC buffer layer and a pre-sintering treatment prior to electrolyte deposition. A full cell with a YSZ electrolyte and LSCF cathode achieved a stable open circuit voltage of approximately 0.7 V and demonstrated continuous operation at 750oC. These findings highlight the suitability of LST-GDC composite anodes as thermochemically stable supports, potentially enabling direct hydrocarbon utilization in intermediate-temperature SOFCs.

  • 298 View
  • 8 Download
A Study on Numerical Thermal Design Techniques for High-power Propulsion Motors
Jaehun Choi, Chiwon Park, Heesung Park
J. Korean Soc. Precis. Eng. 2025;42(11):893-900.
Published online November 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.036

Propulsion motors are vital components in marine propulsion systems and industrial machinery, where high torque and operational reliability are paramount. During operation, high-power propulsion motors generate considerable heat, which can adversely affect efficiency, durability, and stability. Therefore, an effective thermal management system is necessary to maintain optimal performance and ensure long-term reliability. Cooling technologies, such as water jackets, are commonly employed to regulate temperature distribution, prevent localized overheating, and preserve insulation integrity under high-power conditions. This paper examines the cooling performance of water jackets for high-power propulsion motors through numerical analysis. We evaluated the effects of three different cooling pipe locations and varying coolant flow rates on thermal balance and cooling efficiency. Additionally, we analyzed temperature variations in the windings and key heat-generating components to determine if a specific cooling flow rate and pipe configuration can effectively keep the winding insulation (Class H) within its 180oC limit. The findings of this study highlight the significance of optimized cooling system design and contribute to the development of efficient thermal management technologies, ultimately enhancing motor reliability, operational stability, and energy efficiency.

  • 363 View
  • 13 Download

SPECIALs

Development of Droplet Sliding Control Surfaces on Multiscale Hierarchical Polymeric Structures
Min Ji Kim, Seong Min Kim, Ji Seong Choi, Seong Min Kang
J. Korean Soc. Precis. Eng. 2025;42(10):825-832.
Published online October 1, 2025
DOI: https://doi.org/10.7736/JKSPE.D.25.00005

In this paper, we propose a novel method for controlling the anisotropic sliding behavior of droplets using multiscale hierarchical structures. First, we employed a silicon wafer mold containing micro-pillars and directional micro-line structures to induce the directional sliding of droplets. Additionally, we fabricated micro-cone patterns and integrated them into the structures to precisely control droplet movement. These two structures were replicated in polymer and subsequently fused into a single multiscale hierarchical mold through a partial curing process. The completed multiscale hierarchical surface was then replicated with PDMS to create anisotropy that governs the direction of droplet movement. We experimentally confirmed that the degree of sliding is influenced by the cone pattern. Our proposed structural design demonstrates that anisotropic wettability control is achievable even on surfaces made from a single material, indicating potential applications in various fields such as microfluidics, sensors, and functional surfaces.

  • 380 View
  • 11 Download
Emerging Patterning Strategies for Intrinsically Stretchable Conductors: Materials, Architectures, and Device-level Performance
Donghyeon Seo, Seongsik Jeong, Hae-Jin Kim
J. Korean Soc. Precis. Eng. 2025;42(10):789-816.
Published online October 1, 2025
DOI: https://doi.org/10.7736/JKSPE.D.25.00003

Intrinsically stretchable electronics enable seamless integration with dynamic biological tissues and curved surfaces, making them vital for next-generation wearables, biointerfaces, and intelligent robotics. Yet, precise, high-resolution patterning of stretchable electrodes and circuits remains challenging, limiting practical applications. Traditional lithography offers excellent resolution but is hindered by thermal and chemical incompatibilities with soft substrates. Consequently, alternative approaches such as soft lithography, laser-based patterning, printing methods, and electrospray deposition have gained importance. Soft lithography provides an economical, low-temperature option suitable for delicate materials like liquid metals. Laser-based techniques deliver high resolution and design flexibility but require careful parameter tuning for specific substrates. Mask-free printing methods, including direct ink writing and inkjet printing, enable versatile patterning of complex geometries, while electrospray deposition supports precise, non-contact patterning on stretchable surfaces. Collectively, these techniques advance the fabrication of robust stretchable displays, wireless antennas, and bioelectronic interfaces for accurate physiological monitoring. Despite progress, challenges persist, particularly in achieving large-area uniformity, multilayer stability, and sustainable processing. Addressing these issues demands interdisciplinary collaboration across materials science, fluid dynamics, interfacial engineering, and digital manufacturing. This review highlights recent progress and remaining hurdles, offering guidance for future research in stretchable electronics.

  • 268 View
  • 17 Download

REGULAR

Study on UV Energy Effects in High Aspect Ratio Patterning via the Self-propagating Photopolymer Waveguide (SPPW) Method
Jun Ho Song, Woo Young Kim, Seungwoo Shin, Seok Kim, Young Tae Cho
J. Korean Soc. Precis. Eng. 2025;42(9):757-762.
Published online September 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.041

This study quantitatively examines the impact of ultraviolet (UV) intensity and energy on the formation of high aspect ratio (HAR) microstructures using the Self-Propagating Photopolymer Waveguide (SPPW) process. This mechanism relies on the self-focusing of UV light within a refractive index gradient, allowing the light to propagate and polymerize vertically beyond the initial exposure zone. Experiments were performed at UV intensities of 7.5, 12.5, and 17.5 mW/cm2, with energy levels ranging from 0.0375 to 13.5 J/cm2. The results indicated that a lower UV intensity of 7.5 mW/cm2 produced uniform and vertically elongated structures, achieving a maximum aspect ratio of 12.26 at 0.9 J/cm2. In contrast, higher UV intensities led to lateral over-curing, base expansion, and shape distortion, primarily due to rapid polymerization and the oxygen inhibition effect. These findings emphasize the importance of precisely controlling both UV intensity and energy to produce uniform, vertically aligned HAR microstructures, offering valuable insights for optimizing the SPPW process in future microfabrication applications.

  • 273 View
  • 4 Download
Articles
Optimized Microstructures for High Performance Ag/MWCNT/Ecoflex- based Flexible Pressure Sensors
Hyeon Yun Jeong, Jeong Beom Ko
J. Korean Soc. Precis. Eng. 2025;42(8):657-664.
Published online August 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.065
Recently, flexible pressure sensors featuring enhanced sensitivity and durability through nano/micro additive manufacturing have been employed in various fields, including medical monitoring, E-skin technology, and soft robotics. This study focuses on the fabrication and verification of an interdigitated electrode (IDE) based flexible pressure sensor that incorporates microstructures, utilizing a direct patterning-based additive process. The IDE-patterned sample was designed with a total size of 7.95 × 10 mm2, a line width of 150 µm, a spacing of 200 µm, and a probe pad measuring 1.25 × 2 mm2. It was fabricated using AgNP ink on a primed 100 µm thick polyethylene naphthalate (PEN) substrate. The electrode layer was subsequently covered with a sensing layer made of a MWCNT/Ecoflex composite material, resulting in the final pressure sensor sample. Measurements indicated that the sensor exhibited good sensitivity and response speed, and it was confirmed that further improvements in sensitivity could be achieved by optimizing the size, spacing, and height of the microstructures. Building on the flexible pressure sensor structure developed in this study, we plan to pursue future research aimed at fabricating array sensors with integrated circuits and exploring their applicability in wearable devices for pressure sensing and control functions.
  • 287 View
  • 7 Download
Calculation of Flight Loads and Structural Robustness Analysis of Aircraft External Stores Considering Low Speed Rotorcraft Installation
Ji Hwan Park, Chang Bong Ban, Jong Hwan Kim, Sun Kyu Ahn
J. Korean Soc. Precis. Eng. 2025;42(8):613-620.
Published online August 1, 2025
DOI: https://doi.org/10.7736/JKSPE.025.040
External stores on low-speed rotorcraft are subjected to various external forces depending on the aircraft's operating conditions. While there are different types of external forces, this paper focuses on flight loads as defined by US defense specifications. Flight loads consist of static and dynamic loads. Static loads on aircraft external stores include inertial loads resulting from aircraft maneuvers and aerodynamic loads caused by the downward flow of the main wing. To define the inertial load, the inertial load factor on external stores was calculated, while the minimum analysis case for aerodynamic load was derived from trim analysis of rotorcraft blades. The critical design load diagram was developed by combining these factors, and ANSYS was utilized to analyze the structural robustness under static loads. Based on the characteristics of the main wing, a finite element analysis was conducted using a vibration profile tailored to the actual operating environment and an impact profile suitable for the impact conditions. Structural robustness was further assessed through actual tests. This analysis provides essential data for airworthiness certification, allowing for the safe installation of external stores on low-speed rotorcraft.
  • 314 View
  • 10 Download