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Learning About Ares I from Monte Carlo Simulation

机译:从Monte Carlo Simulation了解Ares I

摘要

This paper addresses Monte Carlo simulation analyses that are being conducted to understand the behavior of the Ares I launch vehicle, and to assist with its design. After describing the simulation and modeling of Ares I, the paper addresses the process used to determine what simulations are necessary, and the parameters that are varied in order to understand how the Ares I vehicle will behave in flight. Outputs of these simulations furnish a significant group of design customers with data needed for the development of Ares I and of the Orion spacecraft that will ride atop Ares I. After listing the customers, examples of many of the outputs are described. Products discussed in this paper include those that support structural loads analysis, aerothermal analysis, flight control design, failure/abort analysis, determination of flight performance reserve, examination of orbit insertion accuracy, determination of the Upper Stage impact footprint, analysis of stage separation, analysis of launch probability, analysis of first stage recovery, thrust vector control and reaction control system design, liftoff drift analysis, communications analysis, umbilical release, acoustics, and design of jettison systems.
机译:本文介绍了正在进行的蒙特卡洛模拟分析,以了解Ares I运载火箭的行为并协助其设计。在描述了Ares I的仿真和建模之后,本文介绍了确定必要的仿真所用的过程以及各种参数,以了解Ares I车辆在飞行中的行为。这些模拟的输出为大量设计客户提供了开发Ares I和将搭载在Ares I上的Orion航天器所需的数据。列出客户之后,将描述许多输出示例。本文讨论的产品包括支持结构载荷分析,空气热分析,飞行控制设计,失效/中止分析,确定飞行性能储备,检查轨道插入精度,确定上层撞击足迹,确定阶段分离,发射概率分析,第一阶段恢复分析,推力矢量控制和反作用控制系统设计,升空漂移分析,通讯分析,脐带释放,声学和抛射系统设计。

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