Flame Emission Spectroscopy in a Paraffin-Based Hybrid Rocket
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4564
Reference12 articles.
1. Design and Development of a Thrust Vector Controlled Paraffin/Nytrox Hybrid Rocket
2. Visualization of the Liquid Layer Combustion of Paraffin Fuel for Hybrid Rocket Applications
3. A Visual Study of the Combustion of High-Regression Rate and Classical Hybrid Rocket Fuels
4. Fundamentals of Hybrid Rocket Combustion and Propulsion
5. A technique for improving the performance of hybrid rocket engines
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy;Acta Astronautica;2021-11
2. Development of a Non-intrusive Flame to Fuel Surface Radiative Heat Flux Measurement for Hybrid Rockets;AIAA Propulsion and Energy 2020 Forum;2020-08-17
3. Spectroscopic Techniques for Measuring Regression Rates of Liquefying Hybrid Rocket Fuels;AIAA Propulsion and Energy 2019 Forum;2019-08-16
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