model rocket engine
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2021 ◽  
Vol 33 (6) ◽  
pp. 064108
Author(s):  
Satomi Shima ◽  
Kosuke Nakamura ◽  
Hiroshi Gotoda ◽  
Yuya Ohmichi ◽  
Shingo Matsuyama

2021 ◽  
Vol 2021.27 (0) ◽  
pp. 10A14
Author(s):  
Kazuki KAWANO ◽  
Satomi SHIMA ◽  
Hiroshi GOTODA ◽  
Yuya OHIMICHI ◽  
Shingo MATSUYAMA

2020 ◽  
Vol 12 (3) ◽  
pp. 151-157
Author(s):  
George PELIN ◽  
Cornel STOICA ◽  
Cristina - Elisabeta PELIN ◽  
Raluca BALASA

This paper presents the experimental study of the distillation of hydrogen peroxide to increase the concentration of the solution, in order to use it as rocket fuel in space applications. The process of obtaining the desired concentration required for the operation of the wind tunnel model rocket engine was obtained using the vacuum distillation method. The process consists in removing a calculated value of the water content from the hydrogen peroxide solution with a concentration of 35%, thus increasing its concentration up to the value of 90%. The key factors that contribute in obtaining the desired concentration were evaluated and experimental results were compared with the calculated values.


2020 ◽  
Vol 127 (22) ◽  
pp. 224903 ◽  
Author(s):  
Chinami Aoki ◽  
Hiroshi Gotoda ◽  
Seiji Yoshida ◽  
Shigeru Tachibana

2014 ◽  
Vol 30 (4) ◽  
pp. 978-990 ◽  
Author(s):  
Laurent Selle ◽  
Rodolphe Blouquin ◽  
Marie Théron ◽  
Luc-Henry Dorey ◽  
Martin Schmid ◽  
...  

2014 ◽  
Vol 9 (0) ◽  
pp. 1206001-1206001 ◽  
Author(s):  
Yusuke SASAKI ◽  
Shinji TAKESHITA ◽  
Toru SASAKI ◽  
Takashi KIKUCHI ◽  
Tsukasa ASO ◽  
...  

2013 ◽  
Vol 340 ◽  
pp. 933-936
Author(s):  
Dan Su ◽  
Zhi Hong Zhang ◽  
Jin Ping Zhao

In this paper, we designed a new type of high precision 1 μA constant current source after deeply studying the high precision precise dc constant current source. Compared with the traditional constant current source, in this paper we adopted complex amplifier added with floating power supply outside to design high precision dc constant current source which is for China's space use , its output current is 1 μA, resolution is 0.1 nA, accuracy is 0.5. This high precise dc constant current source is mainly used for new model rocket engine performance testing in aerospace, but also can be widely applied in different fields in need of precision measurement.


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