科技报告详细信息
Additive Manufacturing of Liquid Rocket Engine Combustion Devices: A Summary of Process Developments and Hot-Fire Testing Results | |
Gradl, Paul ; Greene, Sandy ; Protz, Chris ; Bullard, Brad ; Buzzell, James ; Garcia, Chance ; Wood, Jessica ; Cooper, Ken ; Hulka, James ; Osborne, Robin | |
关键词: ADDITIVE MANUFACTURING; COST REDUCTION; ELECTRON BEAMS; HIGH RESOLUTION; REACTIVITY; TECHNOLOGY UTILIZATION; TITANIUM; FABRICATION; LIQUID PROPELLANT ROCKET ENGINES; MANUFACTURING; POWDER (PARTICLES); SINTERING; | |
RP-ID : AIAA Paper 2018-4625,M18-6850 | |
学科分类:航空航天科学 | |
美国|英语 | |
来源: NASA Technical Reports Server | |
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【 摘 要 】
Additive Manufacturing (AM) is an emerging technology with a focus on complex metallic component fabrication: Enables complex shapes and internal features that were not possibly with traditional manufacturing techniques, and significant schedule and overall lifecycle cost reductions. To date at the NASA Marshall Space Flight Center (MSFC), combustion devices component hardware ranging in size from 100 - 35,000 lbf has been designed and manufactured using AM and many of these pieces have been hot-fire tested.
【 预 览 】
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20180006088.pdf | 3940KB | ![]() |