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An Approach to Selection of Material and Manufacturing Processes for Rocket Motor Cases Using Weighted Performance Index

机译:基于加权性能指标的火箭发动机壳体材料和制造工艺选择方法

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Material selection is a very critical design decision, which has a profound influence on the entire development program for rocket motor cases. In the selection process, the main performance parameters and the most appropriate fabrication technology with proven processes must be considered. Many years of practical experience in material selection process with a thorough understanding of materials behavior under various loading environments and hands-on experiences with various available manufacturing processes are of immense help to the design and development engineer for successful completion of the development program. In this paper, an attempt has been made to present an approach for selecting appropriate material and manufacturing process for rocket motor case based on method of Weighted Performance Index (WPI) with the hope that this approach will also provide additional aid to the design engineer for the selection of material and manufacturing process for rocket motor cases. In this method, different properties are assigned a certain weight depending upon their importance to the service requirements. Different properties are normalized using a scaling factor, and finally a weighted property index is computed. The material that scored the maximum numerical value is chosen as the material for fabrication. This approach closely matches with the actual performance. Maraging steel and D6AC are found to be the preferred materials for rocket motor cases for critical missions. HSLA steels are appropriate for less-critical applications, in which rocket motor cases are required in very large numbers (e.g., flow-formed AISI 4130 motor cases~((8))). For the selection of an appropriate manufacturing method, the major parameters considered are dimensional accuracy, cost of production, minimum material waste, and flexibility in design. Again, these properties are given a relative grading, which is then converted into a scaled property. Finally, the weighted performance indices are estimated. The flow-forming method has emerged as the manufacturing method of choice for motor tubes.
机译:材料的选择是一个非常关键的设计决定,它对整个火箭发动机外壳的开发计划有深远的影响。在选择过程中,必须考虑主要性能参数和最合适的制造技术以及经过验证的过程。多年的材料选择过程实践经验,对各种装载环境下的材料行为有透彻的了解,以及各种可用制造过程的动手经验,对设计和开发工程师的成功完成开发计划提供了极大的帮助。在本文中,已经尝试提出一种基于加权性能指数(WPI)方法为火箭发动机壳体选择合适的材料和制造工艺的方法,希望这种方法还将为设计工程师提供额外的帮助。火箭发动机壳体的材料选择和制造工艺。在此方法中,根据不同属性对服务要求的重要性为其分配一定的权重。使用缩放因子对不同的属性进行归一化,最后计算加权属性索引。选择具有最大数值的材料作为制造材料。该方法与实际性能非常匹配。发现马氏体时效钢和D6AC是用于关键任务的火箭发动机外壳的首选材料。 HSLA钢适用于要求非常苛刻的非关键应用场合,在这些场合中需要使用大量的火箭发动机壳体(例如,流动成型的AISI 4130发动机壳体〜((8)))。为了选择合适的制造方法,要考虑的主要参数是尺寸精度,生产成本,最小的材料浪费和设计灵活性。同样,为这些属性指定了相对等级,然后将其转换为缩放属性。最后,评估了加权绩效指数。流动成型方法已经成为汽车电子管的首选制造方法。

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