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Thermal Robustness and Mass Optimization of Heat Pipe Shape for Spacecraft Panel Using a Combination of Response Surface Methodology and Monte Carlo Simulation
応答曲面法とモンテカルロ法を用いたロバスト最適化設計手法(人工衛星用ヒートパイプのロバスト熱性能・質量最適化設計)
2005
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
応答曲面法とモンテカルロ法を用いたロバスト最適化設計手法(人工衛星用ヒートパイプのロバスト熱性能・質量最適化設計)
This paper proposes a practical approach for the robust optimization method using a combination of Design of Experiments (DOE), Response Surface Methodology (RSM) and Monte Carlo Simulation (MCS). This simple practical robust design method can overcome the difficulty of the reliability calculation in terms of procedure and calculation time when compared to previous related other approach. This method was applied to the development of a new heat pipe product for the spacecraft panel, and the
doi:10.1299/kikaib.71.914
fatcat:cdcff6znyrbf5felapz3ztd2qy