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An approach for space launch vehicle conceptual design and multi-attribute evaluation

机译：太空运载火箭概念设计和多属性评估的方法

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摘要

College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;School of Aeronautical Science and Engineering, Beijing University of Aeronautics & Astronautics, XueYuan Road No. 37, Hai Dian District, Beijing, China;School of Aeronautical Science and Engineering, Beijing University of Aeronautics & Astronautics, XueYuan Road No. 37, Hai Dian District, Beijing, China;%This paper presents an approach for space launch vehicle conceptual design and evaluation using multi-attributes decision making analysis. The approach is comprised of morphological matrix method to improve the brain storming process by efficiently identifying potential space launch vehicle design concepts. The potential concepts are screened for compatibility and are then sized for desired mission using Tsiolkovsky ideal velocity rocket equation. The Tsiolkovsky ideal velocity rocket equation supported by mass and propulsion modeling is found to be fast and efficient and is applied for sizing and performance modeling of space launch vehicle at the conceptual design phase. Based on the performance parameters, program related issues and cost attributes, the candidate design concepts are subjected to multi-attribute decision making analysis. This is to rank the alternative design concepts and identify the most promising ones for further considerations. The successful application of the proposed approach in conceptual design and evaluation of space launch vehicle has demonstrated its utility in the early phase of the aerospace system design and decision making.
机译：南京航空航天大学经济与管理学院，南京玉岛街29号，南京210016;南京航空航天大学经济管理学院，南京玉岛街29号，南京210016;经济管理学院，南京航空航天大学，南京玉岛街29号，江苏南京210016;北京航空航天大学航空科学与工程学院，北京市海淀区学园路37号;航空科学与工程学院，北京航空航天大学，北京市海淀区学园路37号；％本文提出了一种利用多属性决策分析方法进行空间运载火箭概念设计和评估的方法。该方法由形态矩阵方法组成，可通过有效识别潜在的太空运载火箭设计概念来改善头脑风暴过程。筛选出可能的概念以确保兼容性，然后使用Tsiolkovsky理想速度火箭方程式确定其大小以进行所需的任务。发现质量和推进模型支持的Tsiolkovsky理想速度火箭方程是快速有效的，并在概念设计阶段用于空间运载火箭的尺寸和性能建模。根据性能参数，与程序有关的问题和成本属性，对候选设计概念进行多属性决策分析。这是为了对替代设计概念进行排名，并找出最有前途的概念以供进一步考虑。提议的方法在航天运载工具的概念设计和评估中的成功应用证明了其在航空航天系统设计和决策的早期阶段的实用性。

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  • 来源
    《Aerospace science and technology》 |2013年第1期|65-74|共10页
  • 作者

    Rizwan Ullah; De-Qun Zhou; Peng Zhou; Mukarrum Hussain; M. Amjad Sohail;

  • 作者单位

    College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;

    College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;

    College of Economics and Management, Nanjing University of Aeronautics & Astronautics, 29 Yudao Street, Nanjing 210016, China;

    School of Aeronautical Science and Engineering, Beijing University of Aeronautics & Astronautics, XueYuan Road No. 37, Hai Dian District, Beijing, China;

    School of Aeronautical Science and Engineering, Beijing University of Aeronautics & Astronautics, XueYuan Road No. 37, Hai Dian District, Beijing, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    space launch vehicle; conceptual design; morphological matrix; performance modeling; cost modeling; multi-attribute decision making;

    机译：太空运载火箭;概念设计;形态矩阵绩效建模;成本建模;多属性决策;

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