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Dynamic Response Analysis of Rocket under Launch Load using Integrated FE Model of Launch Vehicle-Satellite : 발사체-위성 통합 유한요소모델을 이용한 발사하중 하에서 로켓의 동적응답해석

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Authors

김상민

Advisor
김승조
Major
기계항공공학부
Issue Date
2011-02
Publisher
서울대학교 대학원
Keywords
동적응답해석구조 동역학 해석발사체인공위성로켓Dynamic response analysisStructural dynamic analysisLaunch vehicleSatelliteRocket
Description
학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2011.2. 김승조.
Language
eng
URI
https://hdl.handle.net/10371/157421

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