Integrated Simulation Linked with Failure Models for Highly Reliable Design of Liquid Rocket Engine
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概要
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Recently, the new design method is required to predict "system reliability level" at the conceptual design phase, to grasp and to optimize the distribution of "risks and margins" because attainable "system reliability level" strongly depends on its basic concept. This paper describes a sample approach to measure "system reliability level", focusing on analytical modeling of failure mechanism and rocket engine steady-state or dynamic simulator. Some design parameters are picked up to understand where and how their dispersion makes an effect in the whole engine system performance or reliability, and to control the total system robustness.
- THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCESの論文
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 論文
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