Showing results 1 to 7 of 7
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 |
Demonstration of ammonia borane-based hypergolic ignitor for hybrid rocket Jeong, Junyeong; Kim, Kyu-Seop; Bhosale, Vikas Khandu; Kwon, Sejin, ACTA ASTRONAUTICA, v.196, pp.85 - 93, 2022-07 |
Hypergolic ignition delay studies of solidified ethanol fuel with hydrogen peroxide for hybrid rockets John, Jerin; Nandagopalan, Purushothaman; Baek, Seung Wook; Cho, Sung June, COMBUSTION AND FLAME, v.212, pp.205 - 215, 2020-02 |
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 |
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 |
Structural characterization and regression rate of solidified ethanol fuels for hybrid rocket applications John, Jerin; Sharma, Janmejai; Miglani, Ankur; Nandagopalan, Purushothaman; Shaikh, Javed; Baek, Seung Wook, FUEL, v.336, 2023-03 |
고농도 과산화수소 하이브리드 로켓 설계 및 성능 평가 = Design and performance evaluation of hybrid rocket using highly concentrated hydrogen peroxidelink 강신재; Kang, Shinjae; et al, 한국과학기술원, 2016 |
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