| 312 | TEMPERATURE DISTRIBUTION OF METHANOL-HYDROGEN PEROXIDE AUTOTHERMAL REFORMING FOR PEM FUEL CELL IN SPACE EXPLORATION Kwon, Sejin; Park, Byeongseop, 64th International Aeronautical Congress, International Aeronautical Congress, 2013-09-25 |
| 313 | The development of the micro-solid propellant thruster array with improved repeatability Seo, Daeban; Lee, Jongkwang; Kwon, Sejin, JOURNAL OF MICROMECHANICS AND MICROENGINEERING, v.22, no.9, 2012-09 |
| 314 | The effect of heat loss on the burning velocity in a micro combustor Na, Han Bee; Lee, Dae Hoon; Choi, Won Young; Kwon, Sejin, 1st international conference on flow dynamics, 2004-11-11 |
| 315 | The Effect of volume expansion on the flame-vortex interaction Kwon, Sejin, 한국전산유체공학회, pp.78 - 86, 한국전산유체공학회, 1998-01 |
| 316 | The Effect of volume expansion on the Propagation of wrinkled laminar premixed flame Chung, E.H.; Kwon, Sejin, AIAA/ASME/ASEE Joint Propulsion Meeting, AIAA, 1998-01 |
| 317 | The Effect of volume expansion on the propagation of Wrinkled laminar premixed flame Chung, E.H.; Kwon, Sejin, 한국연소학회 1998년도 제17회 KOSCI SYMPOSIUM, pp.139 - 154, The Korean Society of Combustion, 1998-10 |
| 318 | The effect of volume expansion on the propagation of wrinkled laminar premixed flame Chung, EH; Kwon, Sejin, COMBUSTION SCIENCE AND TECHNOLOGY, v.146, no.1-6, pp.85 - 103, 1999 |
| 319 | The effects of motive gas physical properties on the performance of ejector for chemical lasers Jin, J.; Kim, S.; Kwon, H.; Kwon, Sejin, XV International Symposium on Gas Flow, Chemical Lasers, and High-Power Lasers, GCL/HPL 2004, v.5777, pp.155 - 159, 2004-08-30 |
| 320 | The flight test and power simulations of an UAV powered by solar cells, a fuel cell and batteries Lee, Bo Hwa; Park, Poomin; Kim, Keunbae; Kwon, Sejin, JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, v.28, no.3, pp.1137 - 1137, 2014-03 |
| 321 | The flow properties of axi-symmetric annular bell type ejector-jets Park, Gunhong; Kwon, Sejin, 3rd International conference on Flow Dynamics, 2006-11 |
| 322 | The Flow Properties of Axi-Symmetric Annular Bell Type Ejector-Jets Park, Geunhong; Kwon, Sejin, 3rd Asian Joint Conference on Propulsion and Power(AJCPP 2006), 2006-04 |
| 323 | The preparation of a metal foam support of Pt/Al2O3 for combustion of hydrogen Jo, Sungkwon; Jin, Jungkun; Kwon, Sejin, 2008 7th International Workshop on Catalytic Combustion, Paul Scherrer Institut, 2008-09-29 |
| 324 | The proton exchange membrane fuel cell systems using methanolysis of sodium borohydride as a hydrogen source with cobalt catalysts Gang, Byeong Gyu; Kwon, Sejin, INTERNATIONAL JOURNAL OF GREEN ENERGY, v.13, no.12, pp.1224 - 1231, 2016-05 |
| 325 | The Starting Behavior of a Supersonic Ejector Equipped with a Second-Throat Park, Gun Hong; Kwon, Sejin, The Second International Conference of Flow Dynamics, 2005-11 |
| 326 | The The design, fabrication and performance evaluation of a micro catalytic reactor for reforming methanol Kim, Taegyu; Lee, Dae Hoon; Kwon, Sejin, 1st international conference on flow dynamics, 2004 |
| 327 | Thermochemical design of a micro liquid monopropellant rocket with catalytic reaction of hydrogen peroxide Lee, D.H.; Hwang, J.S.; Kwon, Sejin; Park, S.-E., ASME 2002 International Mechanical Engineering Congress and Exposition, IMECE2002, v.4, pp.195 - 200, 2002-11-17 |
| 328 | Thermoelectric power generation using H2O2 decomposition for portable power source Jin, Jungkun; Kwon, Sejin, PowerMEMS 2008, PowerMEMS, 2008-11-09 |
| 329 | Thin Polysilicon Gauge for Strain Measurement of Structural Elements Kim, Yongdae; Kim, Youngdeok; Lee, Chulsub; Kwon, Sejin, IEEE SENSORS JOURNAL, v.10, no.8, pp.1320 - 1327, 2010-08 |
| 330 | Three-Dimensionally Printed Polylactic Acid as Solid Fuel for Hydrogen Peroxide Hybrid Rockets Ahn, Byeonguk; Huh, Jeongmoo; Bhosale, Vikas Khandu; Kwon, Sejin, JOURNAL OF PROPULSION AND POWER, v.37, no.1, pp.171 - 175, 2021-01 |
| 331 | Thrust Characteristics of Axi-Symmetric Annular Bell Type Ejector-Jets Park, Geunhong; Kwon, Sejin, AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, American Institute of Aeronautics and Astronautics, 2007-07-08 |
| 332 | Transient Behavior of H2O2 Thruster: Effect of Injector Type and Ullage Volume An, Sungyong; Brahmi, Rachid; Kappenstein, Charles; Kwon, Sejin, JOURNAL OF PROPULSION AND POWER, v.25, no.6, pp.1357 - 1360, 2009 |
| 333 | Transient behavior of proton exchange membrane fuel cells over a cobalt-phosphorous/nickel foam catalyst with sodium borohydride Gang, Byeong Gyu; Jung, Woosuk; Kwon, Sejin, INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, v.41, no.1, pp.524 - 533, 2016-01 |
| 334 | Transitional behavior of a supersonic flow in a two-dimensional diffuser Kim, S; Kim, H; Kwon, Sejin, KSME INTERNATIONAL JOURNAL, v.15, no.12, pp.1816 - 1821, 2001-12 |
| 335 | TURBULENT PREMIXED HYDROGEN AIR FLAMES AT HIGH REYNOLDS-NUMBERS WU, MS; Kwon, Sejin; DRISCOLL, JF; FAETH, GM, COMBUSTION SCIENCE AND TECHNOLOGY, v.73, no.1-3, pp.327 - 350, 1990 |
| 336 | Viscous potential flow analysis of capillary instability with heat and mass transfer Kim, H. J.; Kwon, Sejin; Padrino, Juan C.; Funada, Toshio, JOURNAL OF PHYSICS A-MATHEMATICAL AND THEORETICAL, v.41, no.33, 2008-08 |
| 337 | Visualization of a constant volume micro combustor for analysis of heat loss and quenching Kim, Sehoon; Na, Hanbee; Lee, Dae Hoon; Kwon, Sejin, 7th FLUCOME, Triennial International Symposium on Fluid Control, Measurement and Visualization, 2003 |
| 338 | Visualization of flame propagation in a constant volume micro combustor Kim, Se Hoon; Na, Han Bee; Lee, Dae Hoon; Kwon, Sejin, 7th FLUCOME, Triennial International Symposium on Fluid Control, Measurement and Visualization, 2003-08-25 |
| 339 | Wafer Coating Process of Cu-based Methanol Steam Reforming Catalysts for Wafer Based MEMS Catalytic Reactor Kim, Taegyu; Lee, Dae Hoon; Yoon, Chun Ho; Kwon, Sejin, The 6th International Symposium on Nanocomposites & Nanoporous Materials, 2005-02 |
| 340 | 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 |
| 341 | 고성능 암모늄 디나이트라마이드 단일추진제를 이용한 마이크로 추력기 = High performance microthruster with ammonium-dinitramide-based monopropellantlink 이도윤; 권세진; et al, 한국과학기술원, 2019 |
| 342 | 과산화수소 단일추진제 추력기를 이용하는 큐브위성 추진 시스템 설계 = Design of CubeSat propulsion system using hydrogen peroxide monopropellant thrusterlink 이승호; 권세진; et al, 한국과학기술원, 2020 |
| 343 | 과산화수소 단일추진제 추력기의 펄스 변조 추력 제어 = Pulse modulation throttling of hydrogen peroxide monopropellant thrusterlink 최석민; 권세진; et al, 한국과학기술원, 2018 |
| 344 | 과산화수소 산화제 하이브리드 로켓 노즐의 삭마 특성 = Characteristics of ablation of hybrid rocket nozzle with hydrogen peroxide as an oxidizerlink 이다혜; Lee, Dahae; et al, 한국과학기술원, 2016 |
| 345 | 과산화수소 하이브리드 로켓을 위한 접촉점화성 고체 연료 개발 및 검증 = Development and validation of hypergolic solid fuel for hybrid rocket with hydrogen peroxidelink 정준영; 권세진; et al, 한국과학기술원, 2020 |
| 346 | 과산화수소/케로신 이원추진제 추력기의 막냉각 연구 Kwon, Sejin; Jang, Donguk; Kwak, Yeongchul, 2013 추계 추진공학회 , 한국추진공학회, 2013-12-05 |
| 347 | 나노 인공위성 적용을 위한 50 mN 급 마이크로 액체 추력기 개발 및 성능 개선 = Development of a 50 mN class liquid micro thruster and performance improvement for nanosatellites applicationslink 허정무; Huh, Jeongmoo; et al, 한국과학기술원, 2016 |
| 348 | 다단 로켓 단분리용 선형 화약 폭굉의 구조 응답 특성 = Structural response for detonation of linear shaped explosive in multistage rocketlink 최승혁; 권세진; et al, 한국과학기술원, 2023 |
| 349 | 단독 추력제어 요소로써의 저독성 접촉점화성 추력기용 핀틀 인젝터의 설계 가능성 검증 = Feasibility study of utilizing pintle injector as sole-throttling device for nontoxic hypergolic thrusterlink 김현탁; 권세진; et al, 한국과학기술원, 2020 |
| 350 | 단일추진제 추력기의 광범위 추력 제어용 이중판 인젝터 시스템 설계 및 성능 평가 = Design and performance evaluation of dual-plate injector for deep throttleable monopropellant thrusterlink 김예현; 권세진; et al, 한국과학기술원, 2021 |
| 351 | 모멘텀 비를 변화한 다중 동축 선회 젯 분사기의 연소 특성에 관한 연구 = Combustion characteristics of multi-element swirl coaxial jet injectors under varying momentum ratioslink 소윤석; 권세진; et al, 한국과학기술원, 2022 |
| 352 | 모바일 연료전지 시스템용 메탄올-과산화수소 산화수증기개질의 특성 = Characteristics of $MeOH-H_2O_2$ oxidative steam reforming for mobile fuel cell applicationslink 박병섭; Park, Byeongseob; et al, 한국과학기술원, 2016 |
| 353 | 무산소 환경 NaBH4/H2O2 직접 연료전지의 친수성 전극 제작과 안정제 농도에 따른 장기 성능 = Hydrophilic electrode and effect of stabilizer concentration on long-term performance of direct NaBH4/H2O2 fuel cell for air independent propulsionlink 장보선; Jang, Bosun; et al, 한국과학기술원, 2015 |
| 354 | 무인기 구동을 위한 PEM 연료전지 스택의 초경량 바이폴라 플레이트 김, 기인; 이, 종광; 김, 태규; 권, 세진; Kim, Kiin; Lee, Jongkwang; Kim, Taegyu; et al, 2011-03-08 |
| 355 | 무인기용 액티브 전력제어장치 개발 및 성능 평가 = Development and performance evaluation of active power management system for UAV'slink 이보화; Lee, Bohwa; et al, 한국과학기술원, 2016 |
| 356 | 새로운 이온성 단일추진제의 합성과 성능 검증 = Novel ionic liquid monopropellant: synthesis and performance validationlink 김주원; 권세진; et al, 한국과학기술원, 2022 |
| 357 | 연료전지 배터리 태양전지를 이용한 무인기용 복합 전기추진 시스템 개발 = Development of a hybrid electrical propulsion system for unmanned aerial vehicles combining the fuel cell with a battery and solar cellslink 강병규; Gang, Byeong Gyu; et al, 한국과학기술원, 2016 |
| 358 | 열을 발생하는 용융물에 대한 냉각전략의 비교연구 = (A) comparative study of cooling strategies for volumetrically heat-generating molten materialslink 나한비; Na, Hanbee; et al, 한국과학기술원, 2017 |
| 359 | 우주 추진용 고성능 친환경 단일추진제 추력기 개발 = Development of high performance green monopropellant thruster for space propulsionlink 백승관; 권세진; et al, 한국과학기술원, 2019 |
| 360 | 우주 추진을 위한 산업용 과산화수소 접촉점화성 하이브리드 추력기 = Industrial grade hydrogen peroxide hypergolic hybrid thruster for in-space propulsionlink 랑성민; Rang, Seongmin; et al, 한국과학기술원, 2023 |
| 361 | 유체진동기 연료 인젝터를 통한 이원추진제 로켓연소기의 연소성능 향상 = Combustion enhancement in a bi-propellant rocket combustor by the fluidic oscillator fuel injectorlink 정상우; 권세진; et al, 한국과학기술원, 2023 |
| 362 | 초음속 충동형 터빈의 부분 분사가 터빈 성능과 진동에 미치는 영향 = Partial admission effect on the performance and vibration of a supersonic impulse turbinelink 이항기; 권세진; et al, 한국과학기술원, 2018 |
| 363 | 친환경 단일추진제 촉매분해 모델링을 이용한 추력기 촉매대 설계 최적화 = Design optimization of green monopropellant thruster catalyst beds using catalytic decomposition modelinglink 정상우; 권세진; et al, 한국과학기술원, 2017 |
| 364 | 친환경 추진제 HAN과 ADN 추력기 개발 Maxime Monette; Kwon, Sejin, 2015년 제45회 한국추진공학회 추계학술대회, 한국추진공학회, 2015-11-27 |
| 365 | 케이싱 트리트먼트를 이용한 천음속 축류 압축기 안정성 향상 = Transonic axial compressor stability enhancement with casing treatmentlink 임병준; Lim, Byeung Jun; et al, 한국과학기술원, 2014 |
| 366 | 터보 냉각 사이클의 고도 모사를 위한 지상 시험 = Ground simulation of altitude test of turbo-refrigeration cyclelink 백승윤; Paek, Seung-Yun; et al, 한국과학기술원, 2017 |
| 367 | 테트라글라임 연료를 이용한 ADN 기반 단일추진제 개발 및 평가 = Development and evaluation of ADN based mono-propellant using tetraglyme fuellink 김주원; 권세진; et al, 한국과학기술원, 2019 |
| 368 | 한국 달 탐사 임무 수행을 위한 궤도 설계 및 분석 Maxime Monette; Lee, Jiho; Kwon, Sejin, 한국항공우주학회 2015 추계학술대회, 한국항공우주학회, 2015-11-19 |
