Closed form formulas for liquid propulsion launch vehicle system reliability

机译：液体推进运载火箭系统可靠性的封闭式公式

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This paper presents the derivation of two closed-form formulas for calculating liquid propulsion launch vehicle system reliability. ^These formulas overcome the inadequacy of some existing formulas and inefficiency of the Monte Carlo simulation and serve as an efficient analytical tool for accurate system reliability evaluation under a given set of input parameter conditions, which in turn greatly helps system-level trade studies and optimization. ^(Author)

机译：本文介绍了用于计算液体推进运载火箭系统可靠性的两个闭式公式的推导。 ^这些公式克服了一些现有公式的不足和蒙特卡洛模拟的效率低下的问题，可作为在给定一组输入参数条件下进行准确系统可靠性评估的有效分析工具，从而极大地帮助了系统级贸易研究和优化。 ^（作者）

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《In: AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 7th, St. Louis, MO, Sept. 2-4, 1998, Collection of Technical Papers. Pt. 3 (A98-39701 10-31), Reston, VA, American Institute of Aeronautics and Astronautics, 1998》|1998年|p1538-1542|共5页
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Huang; Zhaofeng;
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中图分类 V2V4;
关键词
LIQUID PROPELLANTS; LAUNCH VEHICLES; SYSTEM RELIABILITY; COMPUTERIZED SIMULATION; MONTE CARLO METHOD;

机译：液体推进剂;发射车辆;系统可靠性;计算机模拟蒙特卡罗方法;

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Closed form formulas for liquid propulsion launch vehicle system reliability

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