文献类型：期刊文献

英文题名：Review on Impact Loads for Launch Vehicles and Offshore Launch Platform Dynamic Characteristics

作者：Sun, Yifang[1,2];Zhang, Dapeng[1];Wu, Zongduo[1];Yu, Yiquan[3]

机构：[1]Guangdong Ocean Univ, Ship & Maritime Coll, Zhanjiang 524088, Peoples R China;[2]Guangdong Prov Engn Res Ctr Ship Intelligence & Sa, Zhanjiang 524000, Peoples R China;[3]Naval Univ Engn, Dept Naval Architecture, Wuhan 430033, Peoples R China

年份：2026

卷号：14

期号：12

外文期刊名：JOURNAL OF MARINE SCIENCE AND ENGINEERING

收录：SCI-EXPANDED(收录号：WOS:001802592100001)、、EI(收录号：20262621002167)、WOS

基金：This research was funded by the Program for Scientific Research Start-up Funds of Guangdong Ocean University, grant number 060302072102, and the Zhanjiang Marine Youth Talent Project-Comparative Study, grant number 2021E5007.

语种：英文

外文关键词：launch platform; rocket plume; hydrodynamic; motion prediction

外文摘要：Offshore rocket launches offer advantages such as unrestricted launch locations, convenient recovery, large effective payload capacity, and long satellite service life. However, due to the complex marine environment, variations in wind, waves, and currents significantly impact the dynamic performance of the launch platform. The study of rocket plume impact on platforms and the influence of wind, waves, and currents on their dynamic performance, as well as corresponding optimization measures, is of critical importance. This paper provides a comprehensive review of the dynamic issues concerning offshore launch platforms, covering theoretical analysis, numerical simulations, and experimental research. Firstly, the research on rocket plume impact loads is introduced. Subsequently, the research achievements in the hydrodynamic performance, structural dynamics, and motion prediction of launch platforms are summarized. On this basis, recent performance optimization methods for launch platforms are presented. Finally, unresolved issues and future research directions are highlighted. The aim is to offer valuable insights for further advancements in offshore rocket launches.