Zobrazeno 1 - 10
of 25
pro vyhledávání: '"ShinJae Kang"'
Autor:
Shinjae Kang
Publikováno v:
Acta Astronautica. 205:47-56
Autor:
Shinjae Kang, Sanggwan Oh
Publikováno v:
Journal of the Brazilian Society of Mechanical Sciences and Engineering. 45
Publikováno v:
CEAS Space Journal. 13:189-196
In this study, a manganese oxide lanthanum-doped alumina (MnOx/La/Al2O3) catalyst was employed for application in a 95 wt.% hydrogen peroxide thruster. By employing 95 wt.% hydrogen peroxide rather than the conventional 87.5 wt.% hydrogen peroxide, s
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 47:335-343
Autor:
Min-Seok Moon, Joonhyuk Song, Kwang-Seok Kim, Je-Ha Oh, Sung-Mo Yang, ShinJae Kang, MyeongHan Yoo
Publikováno v:
Robotics and Computer-Integrated Manufacturing. 55:154-159
Recently, interest in light-weight vehicle research is spreading swiftly across the globe. This is part of efforts to reduce CO2 emissions in many countries of the world, including developed countries. Magnesium alloys represent light-weight, metalli
Autor:
Sejin Kwon, Shinjae Kang
Publikováno v:
Materials
Volume 14
Issue 11
Materials, Vol 14, Iss 2828, p 2828 (2021)
Volume 14
Issue 11
Materials, Vol 14, Iss 2828, p 2828 (2021)
Spacecraft have monopropellant thruster systems for attitude control in the vacuum of space. Hydroxylamine nitrate is a green propellant that has high performance and low toxicity. Owing to the high adiabatic decomposition temperature of the hydroxyl
Publikováno v:
Fibers and Polymers. 18:1609-1613
Long fiber thermoplastics (LFT) ribs co-molded with woven glass fabric prepregs were considered to design an automotive side impact beam (SIB). The LFT ribs were designed to locate at the center of the continous fiber reinfoced SIB. The woven fabric
Publikováno v:
Acta Astronautica. 130:75-83
The decomposition process of hydrogen peroxide can be applied to a bipropellant thruster, as well as to monopropellant thruster. To provide a framework for the optimal design of the injector and catalyst bed depending on a type of thruster, this rese
Publikováno v:
2018 Joint Propulsion Conference.
Publikováno v:
2018 Joint Propulsion Conference.