rocket motor
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2022 ◽  
Author(s):  
Griffin A. DiMaggio ◽  
Roy J. Hartfield ◽  
Joseph Majdalani ◽  
Vivek Ahuja

Author(s):  
Tian Hui ◽  
Meng Xiangyu ◽  
Zhu Hao ◽  
Li Chengen ◽  
Yu Ruipeng ◽  
...  

2022 ◽  
pp. 107324
Author(s):  
Yin Wang ◽  
Song-qi Hu ◽  
Xue-li Liu ◽  
Lin-lin Liu

Aerospace ◽  
2021 ◽  
Vol 9 (1) ◽  
pp. 1
Author(s):  
Tor Viscor ◽  
Landon Kamps ◽  
Kazuo Yonekura ◽  
Hikaru Isochi ◽  
Harunori Nagata

An understanding of the scalability of hybrid rocket regression models is critical for the enlargement and commercialization of small-scale engines developed within universities and similar research institutions. This paper investigates the fuel regression rates of recent 40 kN thrust-class motor experiments, which were designed based on fuel regression rate correlations of 2.5 kN thrust-class motors from previous research. The results show that fuel regression rates of the 40 kN experiments were within 26% of predictions made using correlations based on 2.5 kN experiments.


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