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The E-3 Test Facility at Stennis Space Center: Research and Development Testing for Cryogenic and Storable Propellant Combustion Systems

机译：斯坦尼斯太空中心的E-3测试设施：低温和可燃推进剂燃烧系统的研发测试

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This paper will provide the reader a broad overview of the current upgraded capabilities of NASA's John C. Stennis Space Center E-3 Test Facility to perform testing for rocket engine combustion systems and components using liquid and gaseous oxygen, gaseous and liquid methane, gaseous hydrogen, hydrocarbon based fuels, hydrogen peroxide, high pressure water and various inert fluids. Details of propellant system capabilities will be highlighted as well as their application to recent test programs and accomplishments. Data acquisition and control, test monitoring, systems engineering and test processes will be discussed as part of the total capability of E-3 to provide affordable alternatives for subscale to full scale testing for many different requirements in the propulsion community.

机译：本文将为读者提供有关NASA约翰·C·斯坦尼斯太空中心E-3测试设施当前升级功能的广泛概述，该设施可对使用液体和气体氧气，气体和液体甲烷，气体氢的火箭发动机燃烧系统和组件进行测试，碳氢化合物燃料，过氧化氢，高压水和各种惰性流体。重点介绍了推进剂系统功能的详细信息及其在最新测试程序和成就中的应用。数据采集和控制，测试监控，系统工程和测试过程将作为E-3总体能力的一部分进行讨论，以为推进界中许多不同的需求提供价格合理的替代方案，以进行小规模的全面测试。

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Pazos, John T.; Chandler, Craig A.; Raines, Nickey G.;
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1. Testing to reach new heights at Stennis Space Center [J] . Patrick Ponticel Aerospace Engineering . 2007,第9期

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2. Liquid Nitrogen Storing and Pressurization Test of a Type Ⅲ Cryogenic Propellant Tank [J] . Sang-Guk Kang, Myung-Gon Kim, Sang-Wuk Park, Key Engineering Materials . 2007,第Pt1期

机译：Ⅲ型低温推进剂罐的液氮储存和加压试验
3. Liquid Nitrogen Storing and Pressurization Test of a Type III Cryogenic Propellant Tank [J] . Sang-Guk Kang, Myung-Gon Kim, Sang-Wuk Park, Key Engineering Materials . 2007,第Pt1期

机译：III型低温推进剂罐的液氮储存和加压试验
4. The E3 Test Facility at Stennis Space Center: Research and Development Testing for Cryogenic and Storable Propellant Combustion Systems [C] . J. Pazos, C. Chandler, N. Raines AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2009

机译：斯坦尼斯航天中心的E3测试设施：低温和可燃推进剂燃烧系统的研发测试
5. Computer simulation of liquid and gaseous propellant run systems for rocket engine component ground test facilities. [D] . deQuay, Laurence. 1992

机译：火箭发动机部件地面测试设施的液体和气体推进剂运行系统的计算机模拟。
6. An advance in transfer line chilldown heat transfer of cryogenic propellants in microgravity using microfilm coating for enabling deep space exploration [O] . J. N. Chung, Jun Dong, Hao Wang, 2021

机译：微杂珠涂层实现微杂物涂层的低温推进剂转移线寒冷传热的进展实现深空探索
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8. E-3 Test Facility at Stennis Space Center: Research and Development Testing for Cryogenic and Storable Propellant Combustion Systems [R] . Pazos, J. T., Chandler, C. A., Raines, N. G. 2009

机译：斯坦尼斯航天中心的E-3测试设施：低温和可存储推进剂燃烧系统的研究和开发测试

The E-3 Test Facility at Stennis Space Center: Research and Development Testing for Cryogenic and Storable Propellant Combustion Systems

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