Browse "School of Mechanical and Aerospace Engineering(기계항공공학부)" by Author Yun, Yongtae
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| Ablation characteristics of rocket nozzle using HfC-SiC refractory ceramic composite Kim, Kyu-Seop; Lee, Sea-Hoon; Nguyen, Van Quyet; Yun, Yongtae; Kwon, Sejin, ACTA ASTRONAUTICA, v.173, pp.31 - 44, 2020-08 |
| Conceptual design of high-speed underwater jet engine using high concentration of hydrogen peroxide Kang, Hongjae; Baek, Seungkwan; Ahn, Byeonguk; Yun, Yongtae; Kwon, Sejin, OCEAN ENGINEERING, v.153, no.1, pp.193 - 200, 2018-04 |
| 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 |
| Design of Multiport Grain with Hydrogen Peroxide Hybrid Rocket Ahn, Byeonguk; Kang, Hongjae; Lee, Eunkwang; Yun, Yongtae; Kwon, Sejin, JOURNAL OF PROPULSION AND POWER, v.34, no.5, pp.1189 - 1197, 2018-09 |
| Development and validation of high-performance hypergolic hybrid rocket fuel ignitor with hydrogen peroxide Jeong, Junyeong; Bhosale, Vikas Khandu; Yun, Yongtae; Kwon, Sejin, 70th International Astronautical Congress (IAC), International Astronautical Federation (IAF), 2019-10-24 |
| Development of 2,500 N class H2O2/HDPE hybrid rocket for lab-scale sounding rocket application Yun, Yongtae; Huh, Jeongmoo; Kim, Youngil; Ahn, Byeonguk; Kwon, Sejin, International Astronautical Congress 2017 (68 th IAC), International Astronautical Federation (IAF), Space Industry Association of Australia, 2017-09-28 |
| Effect of dual-catalytic bed using two different catalyst sizes for hydrogen peroxide thruster Heo, Seonuk; Jo, Sungkwon; Yun, Yongtae; Kwon, Sejin, AEROSPACE SCIENCE AND TECHNOLOGY, v.78, pp.26 - 32, 2018-07 |
| Effect of Fuel Activation Energy on Ignition of Hydrogen Peroxide Hybrid Rocket Yun, Yongtae; Kim, Kyu-seop; Bhosale, Vikas Khandu; Kwon, Sejin, JOURNAL OF SPACECRAFT AND ROCKETS, v.58, no.3, pp.1930 - 1934, 2021-11 |
| Experimental study of ablation characteristics of hafnium-based composites in the hybrid rocket nozzle Kim, Kyu-Seop; Lee, Sea-Hoon; Nguyen, Van Quyet; Yun, Yongtae; Kwon, Sejin, 70th International Astronautical Congress, IAC 2019, International Astronautical Federation, IAF, 2019-10-22 |
| Flight testing of a university based H2O2/HDPE hybrid sounding rocket at KAIST Huh, Jeongmoo; Kim, Youngil; Yun, Yongtae; Ahn, Byeonguk; Kwon, Sejin; Lee, Jaewan; Yoon, Hosung, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, American Institute of Aeronautics and Astronautics Inc, AIAA, 2017-07 |
| Flight testing of an University based H2O2/HDPE Hybrid Sounding Rocket at KAIST Huh, Jeongmoo; Kim, Youngil; Yun, Yongtae; Ahn, Byeonguk; Kwon, Sejin, 2017 Propulsion and energy (53rd JPC), The American Institute of Aeronautics and Astronautics, 2017-07-11 |
| Flight testing of technology demonstrator with hydrogen peroxide hybrid rocket Yun, Yongtae; Seo, Joungki; Park, Kiyun; Jeong, Junyeong; Kim, Juwon; Kwon, Sejin, AIAA Propulsion and Energy Forum and Exposition, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019-08-21 |
| Integration validation of key components for small sounding rockets Yun, Yongtae; Seo, Joungki; Park, Kiyun; Huh, Jeongmoo; Lim, Jaemin; Kwon, Sejin, AEROSPACE SCIENCE AND TECHNOLOGY, v.100, 2020-05 |
| Measurement of Ablations on the Nozzle Throat of Hybrid Rocket Nozzle using 3D-scanning Kim, Kyu-Seop; Yun, Yongtae; Kwon, Sejin, The 9th Kyushu University-KAIST Symposium on Aerospace Engineering, pp.22 - 24, Kyushu University, 2017-12-08 |
| Parametric Study of Solid Fuel for Hydrogen Peroxide Hybrid Rocket Design Yun, Yongtae; Kim, Juwon; Kwon, Sejin, JOURNAL OF PROPULSION AND POWER, v.38, no.2, pp.229 - 240, 2022-03 |
| Port diameter design of multiport solid fuel in hydrogen peroxide hybrid rockets Yun, Yongtae; Huh, Jeongmoo; Kwon, Sejin, AEROSPACE SCIENCE AND TECHNOLOGY, v.110, pp.106485, 2021-03 |
| Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster Huh, Jeongmoo; Jyoti, Botchu V. S.; Yun, Yongtae; Shoaib, M. N.; Kwon, Sejin, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2018-12 |
| Scale-Up Validation of Hydrogen Peroxide/High-Density Polyethylene Hybrid Rocket with Multiport Solid Fuel Yun, Yongtae; Huh, Jeongmoo; Kim, Youngil; Heo, Seonuk; Kim, Hyuntak; Kwon, Sejin, JOURNAL OF SPACECRAFT AND ROCKETS, v.58, no.2, pp.552 - 565, 2021-03 |
| Study of Dual-Catalytic Bed Scale-Up Parameters for High Test Hydrogen Peroxide Thrusters Jung, Sangwoo; Yun, Yongtae; Kwon, Sejin, 70th International Astronautical Congress (IAC), International Astronautical Federation (IAF), 2019-10-24 |
| System integration design based on parametric study of solid fuel in hydrogen peroxide hybrid rocket = 과산화수소 하이브리드 로켓의 고체연료 요소 설계를 기반으로 한 시스템 통합 설계link Yun, Yongtae; Kwon, Sejin; et al, 한국과학기술원, 2021 |
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