Development of the risk oriented program optimization tool (ROPOT) for orbital space plane design concepts

B. Putney, J. Fragola
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引用次数: 2

Abstract

The preliminary design phase of any program is the key to its eventual successful development. The more advanced a design, the more this tends to be true. For this reason, the preliminary design phase is particularly important in the design of aerospace systems. Errors in preliminary design tend to be fundamental and tend to cause programs to be abandoned, or to be changed fundamentally, and at great cost later in the design development. In order to facilitate the identification of attractive design regimes, the NASA Ames Research Center initiated a project, supporting the 2/sup nd/ generation reusable launch vehicle (RLV) Program, to develop an advanced suite of conceptual design tools. The tool, called risk oriented program optimization tool (ROPOT) was developed for evaluation of reusable space transportation system (RSTS) conceptual analysis. The ROPOT tool is a modular "lego-block" approach that is built on risk drivers from the space shuttle. This paper illustrates how this tool was adapted and applied to the decision-making about future space transportation system architectures, including new orbital space plane designs that are to be launched on the new evolved expendable launch vehicles. ROPOT has been further developed to provide the capability to explore crew survival capabilities of the vehicles throughout the mission, and develop insights and concerning the key trades involving performance, cost, crew safety and developmental risk. The tool demonstrated the ability to capture the key trades necessary to make informed decisions concerning alternative vehicle concepts, clearly identify strengths and weaknesses of design alternatives, and identify the most fruitful areas for achieving overall benefits. The results of this effort demonstrate the ability of ROPOT to be easily adapted to evaluate a broad range of vehicle types ranging from fully-reusable advanced concepts of the 2/sup nd/ generation program, to near term expendable vehicles.
面向风险的轨道空间平面设计方案优化工具(ROPOT)的开发
任何项目的初步设计阶段都是其最终成功发展的关键。设计越先进,这种情况就越容易发生。因此,初步设计阶段在航天系统设计中尤为重要。初步设计中的错误往往是根本性的,往往会导致程序被放弃,或者从根本上改变,并在设计开发的后期付出巨大的代价。为了便于确定有吸引力的设计制度,NASA艾姆斯研究中心启动了一个项目,支持2/sup / generation可重复使用运载火箭(RLV)计划,以开发一套先进的概念设计工具。该工具被称为风险导向程序优化工具(ROPOT),用于评估可重复使用空间运输系统(RSTS)的概念分析。ROPOT工具是一种模块化的“乐高积木”方法,建立在航天飞机的风险驱动因素之上。本文说明了该工具如何适应并应用于未来空间运输系统架构的决策,包括将在新发展的一次性运载火箭上发射的新轨道空间平面设计。ROPOT已经进一步发展,以提供在整个任务过程中探索车辆乘员生存能力的能力,并开发涉及性能、成本、乘员安全和发展风险的关键交易的见解。该工具展示了捕捉关键交易所需的能力,以做出有关替代车辆概念的明智决策,清楚地识别设计替代方案的优势和劣势,并确定实现总体效益的最富有成效的领域。这一努力的结果表明,ROPOT能够很容易地适应于评估广泛的车辆类型,从完全可重复使用的先进概念的2/sup和/ generation计划,到近期的消耗性车辆。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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