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우주비행체 적용 단일액체추진제 하이드라진 추력기의 최적설계 및 성능시험평가

정훈 2015년

논문상세정보
    • 저자 정훈
    • 형태사항 26 cm: 삽화: 190 p.
    • 일반주기 지도교수:김정수, 참고문헌 수록
    • 학위논문사항 학위논문(박사)-, 2015. 8, 에너지시스템공학과, 부경대학교 대학원
    • KDC 559, 5
    • 발행지 부산
    • 언어 kor
    • 출판년 2015
    • 발행사항 부경대학교 대학원
    유사주제 논문( 0)
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' 우주비행체 적용 단일액체추진제 하이드라진 추력기의 최적설계 및 성능시험평가' 의 참고문헌

  • 한국추진공학회, 항공우주 추진기관 개론, 한티미디어, 서울
    대한민국 [2008]
  • 이중모드 위상도플러 속도계측기법에 의한 소형 액체로켓엔진 인젝터 분무의 가시화
    권오붕 김정수 배대석 정훈 한국가시화정보학회지, 제8권, 제4호, pp. 60-65 [2010]
  • 우주발사체의 비행자세 3축 정밀제어를 위한 소형 액체로켓엔진의 펄스모드 응답특성
    김정수 김종현 배대석 정훈 한국추진공학회지, 제17권, 제1호, pp. 1-8 [2013]
  • 우주발사체 자세제어용 하이드라진 추력기의 정상상태 추력 특성
    김정수 김종현 정훈 한국추진공학회지, 제16권, 제6호, pp. 48-55 [2012]
  • 액체추진제 추력기의 인젝터 분무 거동에 대한 실험적 연구
    김성초 김정수 김진석 박정 한국항공우주학회지, 제35권, 제9호, pp. 799-804 [2007]
  • 액체의 미립화, 문운당, 서울
    전흥신 대한민국 [2009]
  • 소형 액체로켓엔진 인젝터의 분무 분열특성에 대한 연료분사압력의 영향
    김성초 김정수 박정 정훈 한국추진공학회지, 제11권, 제3호, pp. 50-57 [2007]
  • 소형 액체로켓엔진 인젝터 분무의 연료분사압력 변이에 따른 액적의 공간분포 특성
    김정수 정훈 한국추진공학회지, 제12권, 제5호, pp. 1-8 [2008]
  • 비충돌형 인젝터로부터 발생하는 액체추진제 분무의 준3차원 구조
    김정수 박정 정훈 한국추진공학회지, 제14권, 제6호, pp. 17-24 [2010]
  • 분사압력 및 분사각에 따른 비충돌형 인젝터의 분무특성
    김정수 김종현 정훈 한국추진공학회지, 제16권, 제3호, pp. 1-8 [2012]
  • 미래창조과학부, 외교부, 대한민국 국방부, 안전행정부, 산업통상자원부, 기획재정부, 국토교통부, 해양수산부
    “-2040 우주개발 중장기 계획(제2차 우주개발진흥 기본계획 수정),” Nov. 2013 [2014]
  • 단일액체추진제 소형 추력기의 진공환경 연소시험 및 성능특성 평가
    김정수 한국추진공학회지, 제8권, 제4호, pp. 84-90 [2004]
  • 교육과학기술부, 기획재정부, 외교통상부, 국방부, 행정안전부, 지식경제부, 국토해양부, 국가정보원
    “제2차 우주개발진흥 기본계획,” Dec [2011]
  • 과학기술부, 외교통상부, 국방부, 행정차지부, 산업자원부, 정보통신부, 건설교통부, 해양수산부, 기획예산처
    “Space Vision 제1차 우주개발진흥기본계획,” Jun. 2007 [2016]
  • “충돌형 Doublet 주입기의 설계변수에 따른 분무특성에 관한 연구,”
    김선진 김유 박승운 정해승 한국항공우주학회지, 제22권, 제6호, pp. 8-14 [1994]
  • “초음속 노즐 유동의 최적해석을 위한 난류모델의 평가와 선정,”
    감호동 김정수 한국추진공학회지, 제17권, 제1호, pp. 18-25 [2013]
  • “지상연소시험평가용 추력기 노즐의 성능해석과 형상설계,”
    감호동(Ho Dong Kam) 김정수 배대석 한국추진공학회지, 제16권, 제2호, pp. 10-16 [2012]
  • “준 3차원적 공간분포 계측에 의한 액체추력기 인젝터 연료분무의 분열 및 확산 거동에 관한 연구,”
    김정수 김진석 한국추진공학회지, 제12권, 제5호, pp. 9-17 [2008]
  • “액체로켓용 FOOF와 FOF 인젝터의 분무특성 비교,”
    윤영빈 임병직 정기훈 한국추진공학회지, 제7권, 제2호, pp. 1-6 [2003]
  • “수력파동에 의한 분무변화 및 저주파 연소 불안정에의 영향 예측
    김태균 윤웅섭 이상승 제29회 한국연소학회 추계학술대회, pp. 152-160 [2004]
  • “다목적실용위성 1호 추진시스템 궤도운용 결과 분석,”
    김정수 진익민(Ik-Min Jin) 한조영(Cho-Young Han) 한국추진공학회지, 제4권, 제4호, pp. 107-113 [2000]
  • “고밀도 탄화수소계 연료의 분무 및 연소특성
    문일윤 서성현 임병직 최환석 한영민 한국추진공학회지, 제10권, 제4호, pp. 26-33 [2006]
  • “F-O-O-F 충돌형 Injector의 분무특성 및 혼합성능에 관한 실험적 연구,”
    김유 문덕용 이광진 한국추진공학회지, 제3권, 제3호, pp. 1-8 [1999]
  • www.spacelaunchreport.com
  • www.astronautix.com
  • Zhang, Z. and Ziada, S., “PDA Measurements of Droplet Size and Mass Flux in the Three-dimensional Atomisation Region of Water Jet in Air Cross-flow,” Experiments in Fluids, Vol. 28, N. 1, pp. 29-35, 2000
  • Yi, T. and Santavicca, D.A., “Combustion Instability and Flame Structure of Turbulent Swirl-stabilized Liquid-fueled Combustion," Journal of Propulsion and Power, Vol. 28, No. 5, pp. 1000-1014, 2012
  • Xianguo, L. and Jihua, S., “Experimental Study of Sprays from Annular Liquid Jet Breakup,” Journal of Propulsion and Power, Vol. 15, No. 1, pp. 103-110, 1999
  • Wikipedia, Soyuz, https://en.wikipedia.org/wiki/Soyuz_(rocket_family)
  • Wikipedia, Falcon 9, https://en.wikipedia.org/wiki/Falcon_9
  • Wikipedia, Atlas V, https://en.wikipedia.org/?title=Atlas_V
  • Wernimont, E. J., “System Trade Parameter Comparison of Monopropellants: Hydrogen Peroxide vs Hydrazine and Others," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, CA, USA, AIAA-2006-5235, Jul. 2006
  • United Launch Alliance, Delta Ⅳ Payload Planners Guide, 06H0233, 2007
  • United Launch Alliance, Delta Ⅱ Payload Planners Guide, 06H0214, 2006
  • Tropea, C., Xu, T. H., Onofri, F., Gr han, G., Haugen, P., and Stieglmeier, M., “Dual-mode Phase-Doppler Anemometer,” Particle and Particle Systems Characterization, Vol. 13, No. 2, pp. 165-170, 1996
  • Thunnissen, D., “Chemical Propulsion,” Lecture Note, Jet Propulsion Lab (JPL), Jan. 2000
  • Tanaka, N., Matsuo, T., Furukawa, K., Nishida, M., Suemori, S., and Yasutake, A., “The “Greening” of Spacecraft Reaction Control Systems,” Mitsubishi Heavy Industries Technical Review, Vol. 48, No. 4. pp. 44-50, Dec. 2011
  • Tamaki, N., Shimizu, M., Nishida, K., and Hiroyasu, H., “Effects of Cavitation and Internal Flow on Atomization of a Liquid Jet," Atomization and Sprays, Vol. 8, No. 2, pp. 179-197, 1998
  • Sutton, G.P., History of Liquid Propellant Rocket Engines, AIAA, Reston, VA, USA, 2006
  • Sutton, G. P. and Blblarz, O., Rocket Propulsion Elements, 7th Ed., John Wiley & Sons Inc., New York, NY, USA, 2001
  • Stiesch, G., Modeling Engine Spray and Combustion Processes, Springer, Berlin, Germany, 2003
  • SpaceX, Falcon 9 Launch Vehicle Payload User's Guide, Rev. 1, 2009
  • SpaceX, Falcon 1 Launch Vehicle Payload User's Guide, Rev. 7, 2008
  • Schmidt, E. W., Hydrazine and Its Derivatives: Preparation, Properties, Applications, 2nd ed., Joyn Wiley & Sons, Inc., New York, NY, USA, 2001
  • Sackheim, R. L. and Masse, R. K., "Green Propulsion Advancement-Challenging the Maturity of Monopropellant Hydrazine," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Jose, CA, USA, AIAA 2013-3988, Jul. 2013
  • Ryan, H. M., Anderson, W. E., Pal, S., and Santoro, R. J., “Atomization Characteristics of Impinging Liquid Jets," Journal of Propulsion and Power, Vol. 11, No. 1, pp. 135-145, 1995
  • Rocket & Space Technology, www.braeunig.us
  • Ranz, W. E., “On Sprays and Spraying,” Department of Engineering Research, Pennsylvania State University, Bulletin 65, 1956
  • Portillo, J. E., Collicott, S. H., and Blaisdell, G. A., “Measurements of Axial Instability Waves in the Near Exit Region of a High Speed Liquid Jet,” Physics of Fluids, Vol. 23, No. 12, 124105, 2011
  • Parker, J. M., Thunnissen, D. P., Blandino, J. J., and Ganapathi, G. B., "The Preliminary Design and Status of a Hydrazine MilliNewton Thruster Development," 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, CA, USA, AIAA 99-2596, Jun. 1999
  • Orbital Sciences Corporation, Pegasus User's Guide, Release 7.0, 2010
  • Orbital Sciences Corporation, Minotaur Ⅳ User's Guide, Release 1.1, 2006
  • Miller, K., Sisco, J., Nugent, N., and Anderson, W., “Combustion Instability with a Single-element Swirl Injector," Journal of Propulsion and Power, Vol. 23, No. 5, pp. 1102-1112, 2007
  • McDonell, V. G. and Samuelsen, G. S., “Interlaboratory Comparison of Phase Doppler Measurements in a Research Simplex Atomizer Spray,” Journal of Propulsion and Power, Vol. 10, No. 3, pp. 402-409, 1994
  • Marchione, T., Allouis, C., Amoresano, A., and Beretta, F., “Experimental Investigation of a Pressure Swirl Atomizer Spray,” Journal of Propulsion and Power, Vol. 23, No. 5, pp. 1096-1101, 2007
  • Makled, A. E. and Belal, H., “Modeling of Hydrazine Decomposition for Monopropellant Thrusters," 13th International Conference on Aerospace Sciences and Aviation Technology, ASAT-13-PP-22, 2009
  • Lichtarowicz, A., Duggins, R. K., and Markland, E., “Discharge Coefficients for Incompressible Non-cavitating Flow through Long Orifices,” Journal of Mechanical Engineering Science, Vol. 7, No. 2, pp. 210-219, 1965
  • Li, X. and Shen, J., “Experimental Study of Sprays from Annular Liquid Jet Breakup," Journal of Propulsion and Power, Vol. 15, No. 1, pp. 103-110, 1999
  • Legge, H. and Dettleff, G., “Pitot Pressure and Heat-Transfer Measurements in Hydrazine Thruster Plumes," Journal of Spacecraft, Vol. 23, No. 4, pp. 357-362, 1986
  • Lefebvre, A. H., Atomization and Sprays, Hemisphere Publishing Corp., New York, NY, USA, 1989
  • Law, C. K., “Mechanics of Flame Stabilization in Subsonic and Supersonic Flow,” Major Research Topics in Combustion, Springer, New York, NY, USA, pp. 201-236, 1992
  • Kim, J. S., Park, J., and Kim, S., “Test and Performance Evaluation of Small Liquid-monopropellant Rocket Engines,” 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, CA, USA, AIAA-2006-4388, July 2006
  • Kim, J. S., Kim, J. S., Jung, H., Park, J., Kim, S., and Jang, K. W., “A Study on the Spray Characteristics of a Liquid-Propellant Thruster Injector by PIV/PDA Optical Measurements,” 5th Joint ASME/JSME Fluids Engineering Conference, San Diego, CA, USA, FEDSM2007-37105, Jul.-Aug. 2007
  • Kim, J. S., Jung, H., Kim, J. S., Kim, S., and Yoon, Y., “A Study on the Disintegration Characteristics of Spray Droplets Exiting from a Nozzle Orifice of Liquid-thruster Injector,” International Conference on Computational & Experimental Engineering and Sciences (ICCES), Phuket, Thailand, ICCES0920090101244, Apr. 2009
  • Kim, J. S., Jung, H., Kim, J. S., Kim, S., Park, P., Su, H., and Jang, K. W., “Quasi-3D Visualization of the Dynamic Behavior of Injector-Generated Spray Droplets by Dual-Mode Phase Doppler Anemometry,” The 7th JSME-KSME Thermal and Fluids Engineering Conference, Sapporo, Hokkaido, Japan, Oct. 2008
  • Kim, J. S. and Kim, J. S., "A Characterization of the Spray Evolution by Dual-mode Phase Doppler Anemometry in an Injector of Liquid-propellant Thruster," Journal of Mechanical Science and Technology, Vol. 23, No. 6, pp. 1637-1649, 2009
  • Kim, J. H., Jung, H., and Kim, J. S., “Pulse-mode Performance Characteristics of a Small Liquid-monopropellant Rocket Engine,” 5th European Conference for Aeronautics and Space Sciences (EUCASS 2013), Munich, Germany, A376, July 2013
  • Kesten, A. S., “Analytical Study of Catalytic Reactors for Hydrazine Decomposition," NASA UARL H910461-38, 1969
  • Kent, J. C. and Brown, G. M., “Nozzle Exit Flow Characteristics for Square-edged and Rounded Inlet Geometries," Combustion Science and Technology, Vol. 30, No. 1-6, pp. 121-132, 1983
  • Kenny, R.J., Moser, M.D., Hulka, J., and Jones, G., "Cold Flow Testing for Liquid Propellant Rocket Injector Scaling and Throttling," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, CA, USA, AIAA-2006-4705, Jul. 2006
  • Kato, M., Kano, H., Date, K., Oya, T., and Niizuma, K., “Flow Analysis in Nozzle Hole in Consideration of Cavitation," SAE Technical Paper 970052, 1997
  • Kam, H. D., Kim, J. S., Lee, J. W., and Kim, I. T., “Performance Analysis for the Design Optimization of a Thruster Nozzle Used for Ground Firing Test,” 6th Asian Joint Conference on Propulsion and Power (AJCPP), Xi’an, China, AJCPP2012-143, Mar. 2012
  • Jung, H., Kim, J. S., Kim, J. S., and Park, J., “Effects of Throttling on the Spray Injection Performance in a Small LRE-Injector,” International Conference on Computational & Experimental Engineering and Sciences (ICCES), Phuket, Thailand, ICCES0920090101243, Apr. 2009
  • Jung, H., Kim, J. H., and Kim, J. S., “Test and Evaluation of a 70 N-class Hydrazine Thruster for Application to the Precise Attitude Control of Space Vehicles,” 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Hose, CA, USA, AIAA 2013-3987, July 2013
  • Jung, H., Kim, J. H., and Kim, J. S., “Spray Characteristics under Various Injection Conditions for a Nonimpinging-type Injector Utilized in 70 N-class Hydrazine Thruster,” 6th Asian Joint Conference on Propulsion and Power (AJCPP), Xi’an, China, AJCPP2012-141, Mar. 2012
  • Jung, H., Kim, J. H., and Kim, J. S., “Performance Dependency on the Reaction Chamber L/D (length-to-diameter ratio) of 70 N-class Hydrazine Thruster,” 7th Asian Joint Conference on Propulsion and Power (AJCPP), Jeju, Korea, AJCPP2014-172, Mar. 2014
  • Jung, H. Koo, J. W., Kim, J. S., and Bae, D. S., A Study on the Breakup and Spatial Distribution of Spray Ejected from 4.5 N-class Hydrazine Thruster Injector,” The 8th Asian-Pacific Conference on Aerospace Technology and Science (APCATS2015), Jeju, Korea, 140201(4.6.3), May 2015
  • Johnson, N. L., "The Cause and Consequences of a Satellite Fragmentation: A Case Study," Advances in Space Research, Vol. 23, No. 1, pp. 165-173, 1999
  • JAXA, www.jaxa.jp
  • Inamura, T., Tsutagawa, T., Cho, S. J., and Masuya, G., “Numerical Simulation on the Behavior of a Liquid Jet into an Air Flow,” Heat Transfer-Asian Research, Vol. 30, Issue 6, pp. 473-484, 2001
  • IHI AEROSPACE Co., Ltd., www.ihi.co.jp
  • Hiroyasu, H., “Spray Break-up Mechanism from the Hole-type Nozzle and Its Applications," Atomization and Sprays, Vol. 10, No. 3-5, pp. 511-527, 2000
  • Hill, P. G. and Peterson, C. R., Mechanics and Thermodynamics of Propulsion, 2nd ed., Pearson, New York, NY, USA, 2010
  • Heidmann, M. F., Priem, R. J., and Humphrey, J. C., “A Study of Sprays Formed by Two Impinging Jets," NACA TN 3835, 1957
  • Heidmann, M. F. and Humphrey, J. C., “Fluctuations in a Spray Formed by Two Impinging Jets," NACA TN 2349, 1951
  • Harrje, D. T. and Reardon, F. H., “Liquid Propellant Rocket Combustion Instability," NASA SP-194, 1972
  • Haenlein, A., “Disintegration of a Liquid Jet,” NACA TM 659, 1932
  • Gunder, D. F. and Friant, D. R., "Stability of Flow in a Rocket Motor," Journal of Applied Mechanics (ASME), Vol. 17, No. 3, pp. 327-333, 1950
  • Gordon, S. and McBride, B. J., “Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA RP-1311, 1994
  • Ganippa, L. C., Bark, G., Andersson, S., and Chomiak, J., “Cavitation: A Contributory Factor in the Transition from Symmetric to Asymmetric Jets in Cross-flow Nozzles," Experiments in Fluids, Vol. 36, No. 4, pp. 627-634, 2004
  • Edwards, C. F. and Marx, K. D., “Analysis of the Ideal Phase-Doppler System: Limitations Imposed by the Single-Particle Constraint,” Atomization and Sprays, Vol. 2, No. 3, pp. 319-366, 1992
  • DoD (USA), "Performance Specification (Propellant, Hydrazine)," MIL-PRF-26536F, 2011
  • Delft university of technology, www.lr.tudelft.nl
  • Dantec Dynamics A/S, BSA Flow Software: Version 4, Installation and User’s Guide, Dantec Dynamics A/S, Skovlunde, Denmark
  • Choo, Y. J. and Kang, B. S., “Parametric Study on Impinging-jet Liquid Sheet Thickness Distribution Using an Interferometric Method,” Experiments in Fluids, Vol. 31, No. 1, pp. 56-62, 2001
  • Choi, H. A., Kam, H. D., and Kim, J. S., “Numerical Investigation on the Correlation Between Shock Structure and Thrust Performance in an Overexpanded Nozzle,” 29th Congress of the International Council of the Aeronautical Sciences (ICAS), St. Petersburg, Russia, Sep. 2014
  • Choi, H. A., Bae, S. H., and Kim, J. S., “Flow Characteristics of 2-dimensional Supersonic Nozzle According to Nozzle Pressure Ratio,” 2014 Asia-Pacific International Symposium on Aerospace Technology (APISAT2014), Shanghai, China, Sep. 2014
  • Choi, H. A. and Kim, J. S., “A Numerical Study on the Heat-transfer Characteristics of a Thruster Thermal-barrier Tube,” 7th Asian Joint Conference on Propulsion and Power (AJCPP), Jeju, Korea, AJCPP2014-116, Mar. 2014
  • China Academy of Launch Vehicle Technology, LM-3C User's Manual, 1999
  • China Academy of Launch Vehicle Technology, LM-3B User's Manual, 1999
  • China Academy of Launch Vehicle Technology, LM-3A User's Manual, 1999
  • China Academy of Launch Vehicle Technology, LM-2E User's Manual, 1999
  • Brown, C. D., Spacecraft Propulsion, AIAA, Washington, DC, USA, 1996
  • Bayvel, L. and Orzechowski, Z., Liquid Atomization, Taylor & Francis, Washington, DC, USA, 1993
  • Baumgarten, C., Stegemann, J., and Merker, G. P., “A New Model for Cavitation Induced Primary Break-up of Diesel Sprays," Proceeding of 18th ILASS (Institute for Liquid Atomization and Spray Systems) Europe Conference, Zaragoza, Spain, Sep. 2002
  • Atlas Ⅴ Launch Services User's Guide, Rev. 11, 2010
  • Astrium, http://cs.astrium.eads.net
  • Arianespace, Soyuz CSG User's Manual, Issue 1, Rev. 0, 2006
  • Arianespace, Ariane 5 User's Manual, Issue 5, Rev. 0, 2008
  • Albrecht, H. E., Borys, M., Damaschke, N., and Tropea, C., Laser Doppler and Phase Doppler Measurement Techniques, Springer, Berlin, Germany, 2003
  • Aerojet Rocketdyne, Monopropellant Data Sheets,http://www.rocket.com/propulsion-systems/monopropellant-rockets
  • Aerojet Rocketdyne, Bipropellant Data Sheets, http://www.rocket.com/propulsion-systems/bipropellant-rockets
  • AMPAC-ISP, www.ampacispcheltenham.eu
  • AIAA, Fire, Explosion, Compatibility, and Safety Hazards of Hypergols-Hydrazine, AIAA-SP-084, 1999
  • 70 N급 하이드라진 추력기의 추력실 최적설계와 시험평가
    김정수(Jeong Soo Kim) 김종현(Jong Hyun Kim) 정훈(Hun Jung) 한국추진공학회지, 제18권, 제1호, pp. 42-49 [2014]
  • 70 N급 하이드라진 추력기의 추력실 최적설계와 시험평가
    김정수(Jeong Soo Kim) 김종현(Jong Hyun Kim) 정훈(Hun Jung) 한국추진공학회지, 제18권, 제1호, pp. 50-57 [2014]
  • 70 N급 하이드라진 추력기의 촉매대 형상(L/D) 최적화 연구
    김정수 김종현 정훈 한국추진공학회지, 제17권, 제6호, pp. 30-37 [2013]
  • 1-lbf급 단일액체추진제 로켓엔진의 추력 성능
    김정수 한국추진공학회지, 제8권, 제2호, pp. 32-38 [2004]