摘要: The complex interactions between internal motor generated pressure oscillations and motor structural vibration modes associated with the static test configuration of a Reusable Solid Rocket Motor have potential to generate signifi... 展开
作者 | Nielsen, D. Townsend, J. | ||
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原报告号 | N20050111481 | 总页数 | 24 |
主办者 | National Aeronautics and Space Administration, Huntsville, AL. George C. Marshall Space Flight Center.^National Aeronautics and Space Administration, Washington, DC. | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Space shuttle boosters Solid propellant rocket engines Modal response Surveys Finite element method Oscillations Structural models Design Dynamic loads Vibration Thrust vector control Simulations Testing Validation Mathematical models |