首页> 外文期刊>SAMPE Journal >Composite Payload Fairing Structural Architecture Assessment and Selection
【24h】

Composite Payload Fairing Structural Architecture Assessment and Selection

机译:复合有效载荷整流罩结构设计评估与选择

获取原文
获取原文并翻译 | 示例
           

摘要

This paper provides a summary of the structural architecture assessments conducted and a recommendation for an affordable high performance composite structural concept to use on the next generation heavy-lift launch vehicle, the space launch system (SLS). The structural concepts element of the advanced composites technology (ACT) project and its follow-on the lightweight spacecraft structures and materials (LSSM) project, was tasked with evaluating a number of composite construction technologies for specific Ares Vcomponents: the payload shroud, the interstage, and the core stage intertank. Team studies strived to address the structural challenges, risks and needs for each of these vehicle components. Building on the work from ACT and LSSM, the composites for exploration (CoEx) project is focused on demonstrating composite technologies for a payload fairing for SLS.
机译:本文提供了进行的结构体系结构评估的摘要,并提出了一种可负担得起的高性能复合结构概念的建议,该概念可用于下一代重型运载火箭,空间发射系统(SLS)。先进复合材料技术(ACT)项目及其后续轻型航天器结构与材料(LSSM)项目的结构概念要素的任务是,评估针对特定Ares V组件的多种复合材料建造技术:有效载荷罩,中间级,以及核心阶段的坦克。团队研究致力于解决这些汽车零部件的结构性挑战,风险和需求。基于ACT和LSSM的工作,用于勘探的复合材料(CoEx)项目专注于演示用于SLS的有效载荷整流罩的复合技术。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号