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Launch vehicles conceptual design and structural analysis f an integrated approach via FEM

机译:通过FEM的综合方法进行运载火箭的概念设计和结构分析

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摘要

In this paper a conceptual design methodology for launch vehicles which makes use of a finite element- based structural analysis is developed. The proposed methodology is then tested by applying it to the conceptual design of single stage to orbit (SSTO), vertical take-off and horizontal landing (VTHL), rocket engines powered reusable launch vehicles (RLVs), like Venture Star.
机译:本文提出了一种基于有限元结构分析的运载火箭概念设计方法。然后将该提议的方法应用于单级入轨(SSTO),垂直起飞和水平着陆(VTHL),由火箭发动机提供动力的可重复使用运载火箭(RLV)等概念设计进行测试,例如Venture Star。

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