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Thermal–Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle

机译：可重复使用运载火箭综合低温推进剂储罐概念的热结构优化

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Theodore F. Johnson; W. Allen Waters; Thomas N. Singer; Raphael T. Haftka;
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年度 2008
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1. Simulation Research of Vaporization and Pressure Variation in a Cryogenic Propellant Tank at the Launch Site [J] . Liang Chen, Guo-zhu Liang Microgravity science and technology . 2013,第4期

机译：发射场低温推进剂罐内汽化和压力变化的模拟研究
2. Low-cost titanium propellant tanks for launch vehicle applications [J] . Stainless steel world . 2017,第Apra期

机译：低成本的钛推进剂罐用于发射车辆应用
3. Using Fracture Mechanics Principles for Calculating the Pressurized Structure Lifetime by Example of the Propellant Tank for the Fourth Stage of Launch Vehicle VEGA [J] . A. S. Birukov, V. I. Kalinin, A. V. Grinevich, Solar system research . 2014,第7期

机译：使用断裂力学原理计算运载火箭VEGA第四阶段推进剂箱的受压结构寿命
4. Thermala??Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle [C] . T. Johnson, W. Waters, T. Singer, AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;AIAA Non-Deterministic Approaches Forum;AIAA/ASME/AHS Adaptive Structures Conference;AIAA Gossamer Spacecraft Forum . 2004

机译：可重复使用运载火箭的集成低温推进剂储罐概念的Thermala ??结构优化
5. Advanced metallic thermal protection systems for reusable launch vehicles. [D] . Blosser, Max Leon. 2000

机译：适用于可重复使用运载火箭的先进金属热保护系统。
6. Reusable Non-Invasive and Ultrafast Radio Frequency Biosensor Based on Optimized Integrated Passive Device Fabrication Process for Quantitative Detection of Glucose Levels [O] . Yang Li, Zhao Yao, Wenjing Yue, 2020

机译：基于优化的集成无源器件制造工艺的可重复使用无创和超快射频生物传感器用于定量检测葡萄糖水平
7. Thermal-Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle [O] . Haftka Raphael T., Johnson Theodore F., Waters W. Allen, 2004

机译：可重复使用运载火箭的综合低温推进剂箱概念的热结构优化
8. Thermal-Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle [R] . Johnson, T. F. , Waters, W. A. , Singer, T. N. , 2004

机译：可重复使用运载火箭集成低温推进剂储罐概念的热结构优化

Thermal–Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle

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