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Showing results 1 to 4 of 4

1
Demonstration of 2,500 N class hydrogen peroxide hybrid rocket for lab-scale sounding rocket

YUN, YONGTAE; Huh, Jeongmoo; Kim, Youngil; Kang, Shinjae; Heo, Seonuk; Kwon, Sejin, 2018 Propulsion and energy (54th JPC), The American Institute of Aeronautics and Astronautics, 2018-07-09

2
Demonstration of 2,500 n-class h2o2/hdpe hybrid rocket for lab-scale sounding rocket

Yun, Yongtae; Huh, Jeongmoo; Kim, Youngil; Kang, Shinjae; Heo, Seonuk; Kwon, Sejin, 54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018, American Institute of Aeronautics and Astronautics Inc, AIAA, 2018-07

3
Performance Evaluation of Hybrid Rocket using 95 wt.% H2O2

Kang, Shinjae; Lee, Dahae; Lee, Eunkwang; Kwon, Sejin, 2016 Propulsion and energy(52nd JPC), pp.12, AIAA, 2016-07-26

4
Performance evaluation of lanthanum doped catalyst support for a 50 N hydrogen peroxide thruster

Kang, Shinjae; Kwon, Se-Jin; Kim,Hyuntak; Lee, Dahae, International Aastronautics Congress, The International Astronautical, 2014-09-29

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