首页> 外文会议>International Astronautical Congress >DESIGN APPROACH ADOPTED FOR ENSURING THE STRUCTURAL INTEGRITY OF A HYDRAULIC LINE ASSEMBLY ALONG THE SOLID ROCKET MOTOR FOR A REUSABLE LAUNCH VEHICLE TECHNOLOGY DEMONSTRATION MISSION
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DESIGN APPROACH ADOPTED FOR ENSURING THE STRUCTURAL INTEGRITY OF A HYDRAULIC LINE ASSEMBLY ALONG THE SOLID ROCKET MOTOR FOR A REUSABLE LAUNCH VEHICLE TECHNOLOGY DEMONSTRATION MISSION

机译:用于确保沿固体火箭电动机沿固体火箭电机的结构完整性进行可重复使用的发射车辆技术示范任务的设计方法

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ISRO is planning to demonstrate the reusable launch vehicle (RLV) technology through a Technology Demonstration Vehicle (TDV). A 9 ton Solid Rocket Motor is designed to function as the Booster Motor in this mission. This booster will carry the RLV-TD vehicle through the atmospheric regime. Electrical cables between the base shroud and the avionic packages mounted atop the Motor head end dome are routed along the 9 m length of the Motor using the welded pads over the Motor case, which is a general practice followed in many other Motors. Similarly, a pair of hydraulic lines will be laid along the length of the Motor connecting the control in actuation system in the base shroud and the oil reservoir positioned in the inter-stage. This system consists of a common hydraulic power plant that powers the actuators of both Solid Stage and TDV. The hydraulic fluid circulation to the Booster stage in actuators is through two stainless steel tubes. These tubes are routed over the clamping system placed over the welded pads on the Motor. A cowling assembly protects this assembly from aerodynamic effects in flight. The entire assembly has to be properly integrated to the Motor to take care of the various loads occurring during the ascent phase. The thinner cylindrical shell of the Motor case posed a challenge for this objective. Hence, detailed checks based on analytical and numerical approaches were necessary for ensuring the required margins in various components/sub assemblies. Detailed high fidelity 3-D model of Motor case with segment joint, welded pads, detachable pads, Teflon bush, cowling,fasteners etc. was used for the numerical analysis. Axial dilation of the Motor due to aerodynamic heating, geometric and contact non-linearities etc. were considered in the analysis. Analytical approach was used for estimating the design margins in the welds connecting the welded pad to Motor case using the loads estimated from analysis. This paper describes on the details starting with the configuration design of welded pad, finite element modelling approach, various loads and the analytical/numerical results related to the hydraulic line cowling assembly to ensure the structural integrity of the system under the cumulative loading conditions.
机译:伊罗斯计划通过技术示范车(TDV)来展示可重复使用的发动机(RLV)技术。 9吨固体火箭电机设计成在该任务中作为增压电机起作用。该助推器将通过大气制度携带RLV-TD车辆。在电机头端圆顶上安装的基部护罩和航空封装之间的电缆沿着电机壳体上的电动机沿着电动机的9米长,这是许多其他电动机的一般练习。类似地,一对液压管线将沿着电动机的长度铺设在基部护罩中的致动系统中的电动机的长度和位于级间的储油系统中。该系统包括一个常见的液压电厂,可以为固体阶段和TDV的致动器供电。致动器中的增压级的液压流体循环是通过两个不锈钢管。这些管通过夹紧系统布置在电动机上的焊接焊盘上。穿越整流罩组件可以保护这一组件免受飞行中的空气动力学效果。必须将整个组件适当地集成到电动机上以照顾在上升期间发生的各种负载。电机壳体的较薄的圆柱形外壳为此目的构成了挑战。因此,基于分析和数值方法的详细检查是确保各种组件/子组件中所需的边缘所必需的。使用段接头,焊接垫,可拆卸垫,Teflon Bush,Cowling,紧固件等的电机壳体的详细高保真3-D型号用于数值分析。在分析中考虑了由于空气动力学加热,几何和接触非线性等电机的轴向扩张。分析方法用于使用分析估计的负载估计将焊接焊盘连接到电动机壳体的焊缝中的设计边缘。本文介绍了以焊接焊盘的配置设计,有限元建模方法,各种负载和与液压线穿线组件相关的分析/数值结果开始的细节,以确保系统在累积负载条件下的结构完整性。

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