Development of Regression Formulas for CAMUI Type Hybrid Rockets as Functions of Local O/F-Reference-Cited by-同舟云学术

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Development of Regression Formulas for CAMUI Type Hybrid Rockets as Functions of Local O/F

Published:2010-07-25 Issue: Volume: Page:
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Container-title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Nagata Harunori,Shunsuke Hagiwara,Kaneko Yudai,Wakita Masashi,Totani Tsuyoshi,Uematsu Tsutomu

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. Development of CAMUI hybrid rocket to create a market for small rocket experiments

2. Numerical Simulation of the Flow Field in the Cascaded Multistage Impinging-Jet (CAMUI) Hybrid Rocket

3. Humble, R., Space PropulsionAnalysis andDesign,1sted,McGraw-HillCompanies, Inc., NewYork, 1995, pp.377.

Cited by 5 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. Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines;Aerotecnica Missili & Spazio;2022-05-24

2. Fuel Regression Characteristics of CAMUI type Hybrid Rocket Using Nitrous Oxide;AIAA Propulsion and Energy 2021 Forum;2021-07-28

3. Three-dimensional numerical analysis on combustion performance and flow of hybrid rocket motor with multi-segmented grain;Chinese Journal of Aeronautics;2020-04

4. Error Analysis for CAMUI Type Hybrid Rocket Regression Simulation;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2019

5. Optimum Design CAMUI Type Fuel Grain Shape Using Genetic Algorithm;TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B;2011

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