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Hydraulic Performance  of the Liquid Methane Electric Pump Under Deign and Off-Deign Conditions

Mingyu Jeong, Hyun-Duck Kwak, Hawnil Huh

 

International Journal of Aeronautical and Space Sciences(IJASS) Åõ°í

 

 

È­¼º Âø·ú¼±ÀÇ ÁøÀÔ, ÇÏ°­ ¹× Âø·ú(EDL) °úÁ¤¿¡ ´ëÇÑ ±â¼ú ¹× ¿¬±¸ µ¿Çâ (Part 1 : Entry, Landing, and GN&C)

Technology and Research Trends on Entry, Descent, and Landing(EDL) Process of Mars Landers (Part 1 : Entry, Landing, and GN&C)

¼ÕÁßÈÆ, ÀÌÁ¤Ç×, ÀÌÁÖ¹Ì, ÇãȯÀÏ

2025. 02.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 53±Ç Á¦ 2È£ pp.219-237

 

 Àü±âÆßÇÁ »çÀÌŬ°ú ED ³ëÁñÀ» Àû¿ëÇÑ ¹ß»çü »ó´ÜÀÇ Áß·® ÃßÁ¤ ¿¬±¸

Study on Estimating the Mass of the Upper Stage of a Launch Vehicle Using Electric Pump Cycle and an ED Nozzle

±èÁØ°â, ±è°Ç¿µ, ÀÌÁÖ¹Ì, À̹ÎÈ£, Á¤¹Î±Ô, ÀÌÇüÁø ÇãȯÀÏ

2024. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 52±Ç Á¦ 5È£ pp. 401-413

 

  Ç×°ø¿ìÁÖ ±â¼ú¿¡ ¸®Æ¬ÀÌ¿Â ¹èÅ͸® Àû¿ëÀ» À§ÇÑ ¿ä±¸ Á¶°Ç°ú ÃֽŠµ¿Çâ

Requirements and Trends for the Application of Lithium-Ion Battery in Aerospace Technology

À̹ÎÈ£, ¼ÕÁßÈÆ, ÇãȯÀÏ

2024. 03.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 52±Ç Á¦ 3È£ pp. 209-223

 

»ó´Ü ¾×ü·ÎÄÏ¿£Áø¿ë Åͺ¸ÆßÇÁ ½ÃÇèÀ» À§ÇÑ Åͺ󱸵¿½Ã½ºÅÛ °³¹ß½ÃÇè

Development Test on the Turbine Drive System of Turbopump Test for Upper Stage Liquid Rocket Engines

¿Õ½Â¿ø, ±èÁø¼±, ½É¸íº¸, ±è´ëÁø, ÇãȯÀÏ

2024. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 28±Ç Á¦ 1È£ pp. 67-76, 2024

 

Evaluation of Effective Emissivity Based on Manufacturing and Mounting Scheme for Space-borne Multilayer Insulation

Jungyeom Kim, Jin-Soo Chang, Geon Young Kim, Hwanil Huh

2024. 03.

Journal of Mechanical Science and Technology,Vol. 38, pp. 1497-1506, 2024

 

Experimental Study on Flow Control System of an Electric Pump-Fed Cycle for Thrust Control

Geon Young Kim, Hyoung Jin Lee, Hwanil Huh

2024. 03.

Acta Astronautica. Vol. 216, pp. 44-56

 

Performance Analysis of an Expansion-Deflection Nozzle with Reduced Lengths of Nozzle Extension at a
High-Altitude Environment

Joomi Lee, Junsub Choi, Hwanil Huh

2023. 10.

Journal of Mechanical Science and Technology, 37, pp. 6547-6558, 2023

 

¹èÅ͸® ±â¼ú ¹ßÀü µ¿Çâ°ú Ç×°ø ¿ìÁÖ ÀÓ¹«ÀÇ Àü±â±¸µ¿ ½Ã½ºÅÛ (PART 2 : ¿ìÁÖ ºÐ¾ß Àü±â±¸µ¿ ½Ã½ºÅÛÀÇ ¹èÅ͸® È°¿ë)

Development Trends of Battery Technologies and Electrical-driven System for Aerospace Missions (PART 2 : Battery Utilization in Electrical-driven System for Space Missions)

±è°Ç¿µ, ÀÌÇüÁø, À̹ÎÈ£, ÇãȯÀÏ

2023. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 51±Ç Á¦ 10È£ pp. 709-719

 

¹èÅ͸® ±â¼ú ¹ßÀü µ¿Çâ°ú Ç×°ø ¿ìÁÖ ÀÓ¹«ÀÇ Àü±â±¸µ¿ ½Ã½ºÅÛ (PART 1 : ¸®Æ¬°è¿­ ¹èÅ͸® ¹× Àü±âÃßÁø Ç×°ø±â °³¹ß µ¿Çâ)

Development Trends of Battery Technologies and Electrical-driven System for Aerospace Missions (PART 1 : Development Trends of Lithium based Batteries and Electrified Aircraft Propulsion System)

±è°Ç¿µ, ÀÌÇüÁø, ±èÁØ°â, ÇãȯÀÏ

2023. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 51±Ç Á¦ 10È£ pp. 693-708

 

Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 2: Core technologies)

Donghwi Ha, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee

International Journal of Aeronautical and Space Sciences(IJASS), Vol. 24, pp. 146-165

2023. 08.

https://doi.org/10.1007/s42405-022-00518-8

 

Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1: Performance and Operation)

Donghwi Ha, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee

International Journal of Aeronautical and Space Sciences(IJASS), Vol. 24, pp. 131-145

2023. 08.

https://doi.org/10.1007/s42405-022-00519-7

 

³ëÁñ ±æÀÌ ´ÜÃà ¹æ¾È¿¡ µû¸¥ ED ³ëÁñÀÇ ¼º´É ºÐ¼®

Performance Analysis of an Expansion Deflection Nozzle by Nozzle Length Reduction Method

ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ

2022. 10.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 26±Ç Á¦ 5È£ pp. 11-23

 

Performance analysis of an expansion-deflection(E-D) nozzle based on pintle inflection angle

Junsub Choi, Hwanil Huh

2022. 10.

Journal of Mechanical Science and Technology, Vol. 36, No. 12

 

Development of Ultra Low Specific Speed Centrifugal Pumps Design Method for Small Liquid Rocket Engines

Hye in Kim, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee

Aerospace 2022, 9, 9, 477

2022. 08.

https://doi.org/ 10.3390/aerospace9090477

 

Àü±âÆßÇÁ »çÀÌŬ ¿ìÁÖÃßÁø ÀåÄ¡ÀÇ ¹ëºê ¹× ÆßÇÁ ȸÀü¼ö Á¶Àý¿¡ µû¸¥ Á¤Àû À¯·® °ø±Þ Ư¼º

Static Flow Characteristics of an Electric Pump-fed Cycle Space Propulsion System Using a Valve and Pump RPM Control

±è°Ç¿µ, ÀÌÇüÁø, ±èÁØ°â, ÇãȯÀÏ

2022. 09.

´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 46±Ç Á¦ 9È£ pp. 515-527

 

¿ìÁֹ߻çü »ó´Ü ¿£Áø °³¹ß µ¿Ç⠺м®

Trend Analysis in Upper Stage Engine Development of Space Launch Vehicles

ÇÑ°æȯ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø

2022. 04.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 26±Ç Á¦ 2È£ pp. 79-95

 

±â°è½Ä ÃßÁø ½Ã½ºÅÛ Á¦¾î¸¦ À§ÇÑ °¡½ºÅÍºó ¿£Áø ¸ðµ¨¸µ ¹× ½Ã¹Ä·¹À̼Ç

Modeling and Simulation of a Gas Turbine Engine for Control of Mechanical Propulsion Systems

¹é°æ¹Ì, ÇãȯÀÏ, ±âÀÚ¿µ

2021. 08.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 25±Ç Á¦ 4È£ pp. 43-52

 

¼±¹Ú¿ë MT30 °¡½ºÅÍºó ¿£ÁøÀÇ ¼º´É ¸ðµ¨¸µ¿¡ °üÇÑ ¿¬±¸

Study on Performance Modeling of a MT30 Gas Turbine Engine for Marine Ship Applications

¹é°æ¹Ì, ±âÀÚ¿µ, ÇãȯÀÏ

2021. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 25±Ç Á¦ 1È£ pp. 12-18

 

Àü±âÆßÇÁ »çÀÌŬÀÇ ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ¸ð»ç¿ë ¼ö·ù ½ÃÇè ¿¬±¸

A Study on Water Flow Test for Simulating Propellant Supply System of Electric Pump Cycle

±â¿ø±Ù, Ȳ±â¿µ, ÀÌÀçû, ÃÖÁؼ·, ÇãȯÀÏ, ±è°Ç¿µ

2021. 02.

´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 45±Ç Á¦ 2È£ pp.115-124

 

¾×ü ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛÀÇ Á¤Æ¯¼º ¸ðµ¨¸µ ¹× °ËÁõ

Modeling and Validation of a Liquid Propellant Supply System in Steady States

ÀÌÁÖ¿¬, ±â¿ø±Ù, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø

2020. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 6È£ pp. 143-154

 

¸¶ÇÏ 7 ±ØÃÊÀ½¼Ó Ãæ°ÝÆÄ Åͳο¡¼­ Ç×·Â °¨¼Ò¸¦ À§ÇÑ ÇöóÁ Á¦Æ® ¹ß»ýÀåÄ¡ ¿¬±¸

A Study on Plasma Jet Generator in a Mach 7 Hypersonic Shock Tunnel for Drag Reduction Applications

ÀÌÀçû, ÀÌÀ¯¼®, ÀÌÇüÁø, ÇãȯÀÏ

2020. 11.

´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 44±Ç Á¦ 11È£ pp. 663-671

 

¼ÒÇü¹ß»çü °³¹ß ¹× ÃֽŠ±â¼ú µ¿Çâ

Technology and Development Trends of Small Launch Vehicles

ÃÖÁؼ·, ÇãȯÀÏ, ±â¿ø±Ù

2020. 10.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 5È£ pp. 91-102

 

Performance Analysis and Mass Estimation of a Small-Sized Liquid Rocket Engine with Electric-Pump Cycle

Juyeon Lee, Tae-seong Roh, Hwanil Huh, Hyoung Jin Lee

International Journal of Aeronautical and Space Sciences(IJASS)

2020. 10.

https://doi.org/10.1007/s42405-020-00325-z

 

±ØÃÊÀ½¼Ó È°°ø ºñÇàü(HGV)ÀÇ ¿¬±¸°³¹ß µ¿Çâ

Research and Development Trends of a Hypersonic Glide Vehicle (HGV)

Ȳ±â¿µ, ÇãȯÀÏ

2020. 09

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 48±Ç Á¦ 9È£ pp. 731-743

 

Drag Reduction Analysis of Counterflow Jets in a Short Penetration Mode

Jaecheong Lee, Hyoung Jin Lee, Hwanil Huh

 

Aerospace Science and Technology Vol. 106

2020. 07.

https://doi.org/10.1016/j.ast.2020.106065

 

Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ ·ÎÄÏ ³ëÁñÀÇ µ¿°á ¹× ÆòÇü À¯µ¿ Çؼ® °á°ú¿¡ µû¸¥ ¼º´É Ư¼º

Performance Characteristics of a Rocket Nozzle Based on the KSLV-II According to the Results of Frozen and Equilibrium Flow Analysis

¹®Å¼®, ±èÇѼÖ, ÇãȯÀÏ

2020. 03

´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 44±Ç Á¦ 3È£ pp. 161-168

 

Study on the Combined Effect of Various Injection Conditions on the Drag Reduction by a Counter-flow Jet in Supersonic Flow

Yongchan Kim, Tae-Seong Roh, Hwanil Huh, Hyoung Jin Lee

2020. 03.

Aerospace Science and Technology Vol. 98

https://doi.org/10.1016/j.ast.2019.105580

 

»ó´Ü ÃßÁø ½Ã½ºÅÛ¿¡ Àû¿ëÀ» À§ÇÑ Àü±âÆßÇÁ »çÀÌŬÀÇ ±¹¿Ü ¿¬±¸ µ¿Çâ

Overseas Research Trends of an Electric-Pump Cycle for Application in Upper-Stage Propulsion Systems

±â¿ø±Ù, ÀÌÀçû, ÀÌÇüÁø, ³ëżº, ÇãȯÀÏ

2020. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 24±Ç Á¦ 1È£ pp. 64-77

 

¾×ü ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛÀÇ ¸ðµ¨¸µ ¹× ½Ã¹Ä·¹ÀÌ¼Ç ¿¬±¸ µ¿Ç⠺м®

Research Trend Analysis on Modeling and Simulation of Liquid Propellant Supply System

ÀÌÁÖ¿¬, Â÷½Â¿ø, Çϵ¿ÈÖ, ±â¿ø±Ù, ÀÌÀçû, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø

2019. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 23±Ç Á¦ 6È£ pp. 39-50

 

¹ß»çüÀÇ °íµµº¸Á¤¿ë 3D ÇÁ¸°Æà ȮÀå-±¼Àý ³ëÁñ¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸

Experimental Study on a 3D Printed Altitude-Compensating Expansion-Deflection Nozzle for a Launch Vehicle

À̱âȯ, ¹Ú»óÇö, ±¸ÀÚ¿¹, ÇãȯÀÏ

2019. 12.

´ëÇѱâ°èÇÐȸ ³í¹®Áý B±Ç Á¦ 43±Ç Á¦ 12È£ pp. 859-869

 

 °¡º¯ ÇÉƲ ÀÎÁ§ÅÍ¿¡¼­ ÇÉƲ ÆÁ Çü»ó¿¡ µû¸¥ ºÐ¹«Æ¯¼º ¿¬±¸

Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape

³²Á¤¼ö, ÀÌ°Ç¿õ, ¹Ú¼±Á¤, ÇãȯÀÏ, ±¸ÀÚ¿¹

2019. 09

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 47±Ç Á¦ 9È£ pp. 658-664

 

ÇÉƲ º¯°î °¢µµ¿¡ µû¸¥ E-D ³ëÁñ Ư¼º¿¡ ´ëÇÑ Àü»ê¼öÄ¡Çؼ® ¿¬±¸

Numerical Study on an E-D Nozzle Characteristics with Various Pintle Inflection Angles

¹Ú»óÇö, ¹®Å¼®, ÇãȯÀÏ

2018. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 6È£ pp. 19-27

 

°íµµº¸Á¤ ³ëÁñÀÇ ±â¼ú ¹× ƯÇã µ¿Çâ

Technology and Patent Trends of Altitude Compensation Nozzles

ÃÖÁؼ·, ¹®Å¼®, ÃÖÁ¾ÀÎ, ¹Ú»óÇö ±èÇѼÖ, ÇãȯÀÏ

2018. 08

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 46±Ç Á¦ 8È£ pp. 662-670

 

µà¾ó º§ ³ëÁñÀÇ ¼³°è º¯¼ö¿¡ µû¸¥ õÀÌ Æ¯¼º

Transition Characteristics with Design Parameters of Dual Bell Nozzle

±èÁ¤ÈÆ, ÇãȯÀÏ

2018. 07.

´ëÇѱâ°èÇÐȸ³í¹®Áý B±Ç Á¦ 42±Ç Á¦7È£ pp. 503-511

 

1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ 2Ãà ÇÉƲ Ã߷±⠽ýºÅÛÀÇ ¾Ð·Â°­ÇÏ Æ¯¼º ºÐ¼®

Analysis of Pressure Drop in Two-Axis Pintle Thrusters Using 1-D Simulation

ÀÌÀçû, ÇãȯÀÏ

2018. 03.

´ëÇѱâ°èÇÐȸ³í¹®Áý B±Ç Á¦ 42±Ç Á¦ 3È£ pp. 177-186

 

 

ÃÊÀ½¼Ó ȯ°æ¿¡¼­ ¿ªºÐ»ç °ø±â Á¦Æ®ÀÇ ¾Ð·Â º¯È­¿¡ µû¸¥ À¯µ¿ Ư¼º ¹× Ç×·Â °¨¼Ò

Flow Characteristics and Drag Reduction with Different Pressures of Counterflow Air Jets in Supersonic Flow

ÃÖÁ¾ÀÎ, ÀÌÀçû, °­½Â¿ø, ÇãȯÀÏ

2018. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 1È£ pp. 58-65

 

µà¾ó º§ ³ëÁñ°ú E-D ³ëÁñÀ» °áÇÕÇÑ Çѱ¹Çü¹ß»çüÀÇ ºñÃß·Â Áõ°¡

Specific Impulse Gain for the KSLV-II with Combination of Dual Bell Nozzle and E-D Nozzle

¹®Å¼®, ÇãȯÀÏ

2018. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 22±Ç Á¦ 1È£ pp. 16-27

 

ÇöóÁ ºÐ»çÀåÄ¡¸¦ È°¿ëÇÑ ÃÊ°í¼Ó ºñÇàüÀÇ Ç׷°¨¼Ò ±âÃÊ ½ÇÇè

Fundamental Experiments of Drag Reduction for a High Speed Vehicle Using Plasma counterflow Jets

°­½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ

2017. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 6È£ pp.57-63

 

°íµµ º¸Á¤¿ë È®Àå-±¼Àý(E-D) ³ëÁñÀÇ ±¹¿Ü ¿¬±¸ µ¿Çâ

Research Trends of an E-D Nozzle for Altitude Compensation

¹®Å¼®, ¹Ú»óÇö, ÃÖÁؼ·, ÇãȯÀÏ

2017. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 45±Ç Á¦ 10È£ pp.844-854

 

ÆØâºñ°¡ °íÁ¤µÈ µà¾ó º§ ³ëÁñÀÇ ÃµÀÌƯ¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸

Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed

ÃÖÁؼ·, ÇãȯÀÏ

2017. 06.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 3È£ pp.68-75

 

³ëÁñ ¸ñ ³»ºÎÇü ÇÉƲÃ߷±âÀÇ Ãß·Â ¹× °ø·ÂÇÏÁß Æ¯¼º

Thrust and Aerodynamic Load Characteristics of an Internal Pintle Thruster

ÃÖÁؼ·, ±èµ¿¿¬, ÇãȯÀÏ

2017. 06.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 21±Ç Á¦ 3È£ pp.1-9

 

Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems

Yeerang Lim, Jaecheong Lee, Hyochoong Bang, Hwanil Huh, Hosung Lee

2017. 05.

International Journal of Aerospace Engineering Vol.2017

https://doi.org/10.1155/2017/4104212

 

Numerical Study for Flame Deflector Design of a Space Launch Vehicle

Hwayoung Oh, Jungil Lee, Hyungsik Um, Hwanil Huh

2017. 04.

Advances in Space Research Vol.59 No.7 pp.1833~1847

https://doi.org/10.1016/j.asr.2016.12.038

 

ÃÊ°í¼Ó ºñÇàü Ç×·Â °¨¼Ò¸¦ À§ÇÑ ÇöóÁ ºÐ»çÀåÄ¡¿¡ ´ëÇÑ ¿¹ºñ °á°ú

Preliminary Results on Plasma Counterflow Jets for Drag Reduction of a High Speed Vehicle

°­½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ

2016. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 20±Ç Á¦ 6È£ pp.101-112

 

Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÑ µà¾ó º§ ³ëÁñÀÇ Àü»ê¼öÄ¡Çؼ® ±âÃÊ °á°ú

Preliminary CFD Results of a Dual Bell Nozzle based on the KSLV-II

±èÁ¤ÈÆ, ÃÖÁؼ·, ÇãȯÀÏ

2016. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 20±Ç Á¦ 6È£ pp.18-28

 

°íµµ º¸Á¤¿ë E-D ³ëÁñÀÇ Ã߷ Ư¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸

Numerical Study on Thrust Characteristics of an E-D Nozzle for Altitude Compensation

ȲÈñ¼º, ÇãȯÀÏ

2016. 06.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 20±Ç Á¦ 3È£ pp.87-95

 

ÇÉƲ ±¸µ¿¼Óµµ¿¡ µû¸¥ ÇÉƲ Ã߷±âÀÇ ºñÁ¤»ó»óÅ Ư¼º¿¡ ´ëÇÑ ½ÇÇèÀû ¿¬±¸

Experimental Study on Unsteady-state Characteristics of a Pintle Thruster with Variable Pintle Speeds

ȲÈñ¼º, ÇãȯÀÏ

2016. 03.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 3È£ pp.247-255

 

¿­Áø°ø è¹ö¿ë Æóȸ·Î ¿­Á¦¾î½Ã½ºÅÛ ¼³°è ¹× ¼º´ÉÆò°¡

Design and Performance Test of a Closed Loop Thermal Control System for Thermal Vacuum Chamber

¼­ÈñÁØ, Á¶ÇõÁø, ¹Ú¼º¿í, ¹®±Í¿ø, Á¤»óÇå, ÇãȯÀÏ

2016. 01

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 1È£ pp.88-97

 

ÃÊ°í¼Ó ºñÇàü Ç׷°¨¼Ò¸¦ À§ÇÑ ¹Ì±¹ÀÇ ºÐ»ç Á¦Æ® ¿¬±¸ µ¿Çâ°ú ÇÙ½É º¯¼ö

Key Parameters and Research Review on Counterflow Jet Study in USA for Drag Reduction of a High-speed Vehicle

±èÁöÈ«, °­½Â¿ø, ÀÌÀçû, ÇãȯÀÏ

2016. 01.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 44±Ç Á¦ 1È£ pp.23-32

 

ÀÜ¿©ÃßÁøÁ¦ ÃßÁ¤À» À§ÇÑ ¿­Áú·®¹ýÀÇ Åë°èÀû ºÒÈ®½Ç¼º ºÐ¼®

Statistical Uncertainty Analysis of Thermal Mass Method for Residual Propellant Estimation

¹ÚÀÀ½Ä, ¹ÚºÀ±Ô, ÇãȯÀÏ

2015. 12.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1116-1123

 

¿À¸®Çǽº¿¡¼­ ±âüÀÇ Ç¥ÁØÀ¯·®À» ÀÌ¿ëÇÑ »ê¼Ò¿Í Çï·ýÀÇ ´©¼³·® ÃøÁ¤¿¡ °üÇÑ ¿¬±¸

Study on Leakage Measurements of Oxygen and Helium Using Standard Gas Flow Rates in a Orifice Flow

ÀÌÁß¿±, ÇÑ»ó¿±, ÇãȯÀÏ

2015. 12.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1108-1115

 

³ëÁñ ¸ñ ¿ÜºÎÇü ÇÉƲÃ߷±âÀÇ Ãß·ÂƯ¼º¿¡ ´ëÇÑ ¼öÄ¡Çؼ® ¿¬±¸

Numerical Study on Thrust Characteristics of an External Pintle Thruster

ÃÖÁؼ·, ±èµ¿¿¬, ÇãȯÀÏ

2015. 12.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 12È£ pp.1071-1078

 

¿­Áø°ø è¹ö¿ë ±ØÀú¿Â ºí·Î¿ö ¼³°è ¹× ¼º´ÉÆò°¡

Design and Performance Tests of a Cryogenic Blower for a Thermal Vacuum Chamber

¼­ÈñÁØ, Á¶ÇõÁø, ¹Ú¼º¿í, ¹®±Í¿ø, ÇãȯÀÏ

2015. 11.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 11È£ pp.1008-1015

 

µ¶ÀÏ DLRÀÇ µà¾ó º§ ³ëÁñ Ư¼º ¹× ÇÙ½É º¯¼ö

Characteristics and Key Parameters of Dual Bell Nozzles of the DLR, Germany

±èÁ¤ÈÆ, ÇãȯÀÏ

2015. 11.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 11È£ pp.952-962

 

´ÙÃà ÇÉƲ Ã߷±⿡ Àû¿ëÀ» À§ÇÑ ±¸µ¿ÀåÄ¡ ¿¬µ¿ ¸ÞÄ¿´ÏÁò ¹æ¾È¿¬±¸

Study on Coupling Drive Mechanism for Multi-Axis Pintle Thrusters

ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º

2015. 08.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 8È£ pp.722-730

 

°íµµ º¸Á¤¿ë µà¾ó º§ ³ëÁñ °³¹ß µ¿Çâ°ú ±â¼ú ºÐ¼®

Technology Review and Development Trends of Dual-Bell Nozzle for Altitude Compensation

ÃÖÁؼ·, ÇãȯÀÏ

2015. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 5È£ pp.456~465

 

1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ ÇÉƲÃ߷±âÀÇ ¼º´ÉÇؼ® - II : ºñÁ¤»ó»óÅ Ư¼º

Performance Analysis of the Pintle Thruster Using 1-D Simulation - II : Unsteady State Characteristics

³ë¼ºÇö, ±èÁöÈ«, ÇãȯÀÏ

2015. 04.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 4È£ pp.311~317

 

1-D ½Ã¹Ä·¹À̼ÇÀ» È°¿ëÇÑ ÇÉƲÃ߷±âÀÇ ¼º´ÉÇؼ® - I : Á¤»ó»óÅ Ư¼º

Performance Analysis of the Pintle Thruster Using 1-D Simulation - I : Steady State Characteristics

±èÁöÈ«, ³ë¼ºÇö, ÇãȯÀÏ

2015. 04.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 4È£ pp.304~310

 

¸óÅ×Ä«¸¦·Î¹æ¹ýÀ» ÀÌ¿ëÇÑ Ãµ¸®¾ÈÀ§¼º ±ËµµÀüÀÌ ¼Ò¿äÃßÁøÁ¦·® ÃßÁ¤¿¡ °üÇÑ ¿¬±¸

COMS GTO Injection Propellant Estimation using Monte-Carlo Method

¹ÚÀÀ½Ä, ÇãȯÀÏ

2015. 01.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 43±Ç Á¦ 1È£ pp.62~71

 

Çѱ¹Çü¹ß»çü ¹ß»ç´ë½Ã½ºÅÛ È­¿°À¯µµ·Î °³³ä ¼³°è (I)

Conceptual Design of KSLV-II Launch Complex Flame Deflector

¿ÀÈ­¿µ, °­¼±ÀÏ, ±è´ë·¡, ÀÌÁ¤ÀÏ, ¾öÇü½Ä, ÇãȯÀÏ

2014. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 18±Ç Á¦ 6È£ pp.75~81

 

Á¤Áö±ËµµÀ§¼ºÀÇ ÀÜ¿©ÃßÁøÁ¦·® ÃøÁ¤¹æ¹ý ¹× ±â¼úµ¿Çâ

Residual Propellant Gauging Methods for Geostationary Satellites and Recent Technology Status

¹ÚÀÀ½Ä, ÇãȯÀÏ

2014. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 42±Ç Á¦ 10È£ pp.870~877

 

¿ìÁÖ ¿­È¯°æ ¸ð»ç¿ë ¼ÒÇü ±ØÀú¿Â ºí·Î¿ö ¼³°è ¹× ¼º´ÉÆò°¡

Design and Performance Test of a Cryogenic Blower for Space Thermal Environment Simulation

¼­ÈñÁØ, ¾È¼º¹Î, ÇãȯÀÏ

2013. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 41±Ç Á¦ 10È£ pp.833~839

 

Áß¾Ó ºÐ»ç ¹æ½Ä ³Ã°¢¼ö ÅõÀÔ¿¡ ÀÇÇÑ ·ÎÄÏ ¿¬¼Ò ÈÄ·ù ³Ã°¢¿¡ °üÇÑ ¿¬±¸

A Study for Rocket Exhaust Flow Cooling due to the Central Spray Type Water Injection

°­¼±ÀÏ, ³²Áß¿ø, ÇãȯÀÏ

2013. 07

Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø Ç×°ø¿ìÁÖ±â¼ú Á¦ 12±Ç Á¦ 1È£ pp.163~172

 

±ËµµÃµÀÌ ¹× ÀÚ¼¼Á¦¾î ½Ã½ºÅÛÀÇ ¿¬±¸°³¹ß µ¿Çâ°ú Àü¸Á

Recent Progress in R&D and Prospect of Divert and Attitude Control System(DACS)

±è¼º¼ö, ÇãȯÀÏ

2012. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 16±Ç Á¦ 6È£ pp.62~72

 

´ÜÀÏÈ­ÇÐÁ¾ ºñ¹ÝÀÀ Çؼ® ¸ðµ¨À» »ç¿ëÇÑ ·ÎÄÏ ¿¬¼ÒÈÄ·ù À¯µ¿Çؼ® ¿¬±¸

A CFD Study for Rocket Exhaust Flow using Single Species, Unreacted Flow Model

°­¼±ÀÏ, ÇãȯÀÏ

2012. 07.

Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø Ç×°ø¿ìÁÖ±â¼ú Á¦ 11±Ç Á¦ 1È£ pp.126~134

 

Àú±Ëµµ À§¼º °úÇОÀçüÀÇ ¿­Çؼ® ¸ðµ¨ °ËÁõÀ» À§ÇÑ ¿­¸ðµ¨ º¸Á¤ ¹× È÷ÅÍ ¼³°è

Thermal Model Correlation and Heater Design Verification for LEO Satellite Optical Payload's Thermal Analysis Model Verification

±è¹ÎÀç, ÇãȯÀÏ, ±è»óÈ£, Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø

2011. 11.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 39±Ç Á¦ 11È£ pp.1069~1076

 

¾×ü·ÎÄÏ¿£ÁøÀÇ À¯·®Á¶Àý¿¡ °¡º¯¹ëºêÀÇ Á¶Àý±â¹ý°ú Ç÷±Àú Çü»óÀÌ ¹ÌÄ¡´Â ¿µÇâ

Effect of Control Method and Plunger Profile of Variable Valve on Flow Control of a Liquid Rocket Engine

ÀÌÁß¿±, ÇãȯÀÏ

2011. 10.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç Á¦ 5È£ pp.35~47

 

Analysis of formation and breakup mechanisms in rotary atomization through spray visualization

Donghun Lee, Gyungwon You, Seongman Choi, Hwanil Huh

2011. 06.

Journal of visualization

https://doi.org/10.1007/s12650-011-0087-9

 

Àú±ËµµÀ§¼º ±¤ÇОÀçüÀÇ Áö»ó ¿­Áø°ø ½ÃÇèÀ» À§ÇÑ ¿¹ºñ ¿­Çؼ®

Preliminary Thermal Analysis for LEO Satellite Optical Payload's Thermal Vacuum Test

ÀÌÁ¾·ü, ÇãȯÀÏ, ±è»óÈ£, Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø

2011. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 39±Ç 5È£ pp.466~473

 

¸¶ÀÌÅ©·Î µ¿·Â¹ß»ý¿ë ¼ÒÇü ½ºÀ§½º·Ñ ¿¬¼Ò±âÀÇ Å©±â¿Í Çü»ó È¿°ú¿¡ ´ëÇÑ ¿¬±¸

Effect of Scale and Geometry on the Performance of Heat-Recirculating Swiss roll combustors for Micro Power Generation Applications

¿ÀÈ­¿µ, ÇãȯÀÏ, Paul D. Ronney

2011. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç 1È£ pp.1~10

 

ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ¼º´É Çâ»ó¿¡ °üÇÑ ¿¬±¸

Study of Thrust Control Performance Improvement for Hybrid Rocket Applications

ÃÖÀ缺, °­¿Ï±Ô, ÇãȯÀÏ

2011. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 15±Ç 1È£ pp.55~62

 

¿¬·áÀüÁö °³Áú±â·Î È°¿ëÀ» À§ÇÑ ½ºÀ§½º ·Ñ ¿¬¼Ò±âÀÇ Å©±â¿Í ¿¬·áÀÇ Á¾·ù¿¡ µû¸¥ Ư¼º¿¬±¸

Effect of Scale and Fuel Type on Heat-recirculating Swiss-roll Combustor Performance for Fuel Cell Reformer Applications

±è¿¬È£, ÇãȯÀÏ, Paul D. Ronney

2011. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 6È£ pp.11~18

Çѱ¹°úÇбâ¼ú´ÜüÃÑ¿¬ÇÕȸ - °úÇбâ¼ú¿ì¼ö³í¹®»ó ¼ö»ó! (2011³â 7¿ù 5ÀÏ)

Àü±âÃßÁø 1Åæ±Þ Personal Air VehicleÀÇ µ¿·Â½Ã½ºÅÛ ¿¹ºñ ºÐ¼®

Preliminary Analysis of Power Systems for 1-ton class Electric Powered PAV

À±µ¿ÀÍ, ÇãȯÀÏ, ¾ç¼ö¼®

2010. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 6È£ pp.1~8

 

°¡½º¹ß»ý±â ¿¬·á°³Æó¹ëºêÀÇ µ¿Àû °Åµ¿

Dynamic Characteristics for Fuel Shutoff Valve of a Gas Generator

ÀÌÁß¿±, ÇãȯÀÏ

2010. 08.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 4È£ pp.1~9

 

UAV ÃßÁø±â°üÀÇ Á¾·ù ¹× Ư¼º¿¡ °üÇÑ ±â¼úÀû °íÂû

Technical Survey on the Classification and Characteristics of UAV's Power Plants

À̵¿ÈÆ, Æر⼮, ±èÀ¯ÀÏ, ¹ÚºÎ¹Î, ÃÖ¼º¸¸, ÇãȯÀÏ

2010. 06.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 3È£ pp.79~86

 

ÀΰøÀ§¼º žÀçÇ° ¼öÁØ ¿­Áø°ø ½ÃÇè¿¡ ´ëÇÑ ¿­Çؼ® ¸ðµ¨ÀÇ °³¹ß°ú ȯ°æ½ÃÇè °á°ú¸¦ ÀÌ¿ëÇÑ °ËÁõ

Development and verification of Thermal Analysis Model for Thermal vacuum Test of Satellite Components

±è»óÈ£, ¼­Çö¼®, À¯ÀçÈ£, ÇÑÀº¼ö, ±èÅ°æ, ±èÇüµ¿, ÇãȯÀÏ

2010. 08.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 38±Ç 8È£ pp.842~847

 

GO2/PE ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î¸¦ À§ÇÑ ½Ã½ºÅÛ ¼³°è ¹× ±âÃʽÇÇè

Sytem Design and Fundamental Experiment for Thrust Control of GO2/PE Hybrid Rocket

ÀÌ¿ë¿ì, °­¿Ï±Ô, ÇãȯÀÏ

2010. 02.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 14±Ç 1È£ pp.40~47

 

°¡½º¹ß»ý±â »êÈ­Á¦ °³Æó¹ëºêÀÇ ³»ºÎ À¯µ¿Æ¯¼º ¹× ±¸Á¶Çؼ®¿¡ °üÇÑ ¿¬±¸

Study on Flow Property and Structural Analysis of Gas Generator Oxidant On/Off valve

ÀÌÁ¾·ü, ÇãȯÀÏ, ¾È¾ç¿ì

2009. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 13±Ç 6È£ pp.48~55

 

Personal Air VehicleÀÇ ÃßÁø½Ã½ºÅÛ¿¡ ´ëÇÑ ±â¼úÀû °íÂû

Thchnical Survey on Propulsion Systems for Personal Air Vehicles

À±µ¿ÀÍ, ÇãȯÀÏ

2009. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 13±Ç 6È£ pp.56~63

 

µå·³Çü ȸÀü¿¬·á³ëÁñÀÇ ¹Ì¸³È­ ±â±¸ ¹× ºÐ¹«Æ¯¼º ¿¬±¸

The Atomization Mechanism and Spray Characteristics of Drum Type Rotary Atomizer

À̵¿ÈÆ, ÃÖÇö°æ, ÃÖ¼º¸¸, À¯°æ¿ø, ÇãȯÀÏ

2008. 04.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 12±Ç 2È£ pp.57~65

 

¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ Àû¿ëÀ» À§ÇÑ ´©¼¾¼ö¿¡ µû¸¥ ¿­Àû¹ß»ê¿ø¸®ÀÇ È¿À²ºÐ¼®

Efficiency Analysis of Thermal Transpiration According to Knudsen Number for Application to Micro-propulsion System

Á¤¼ºÃ¶, ÇãȯÀÏ

2008. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 36±Ç 5È£ pp.483~490

 

¼¼Â÷Á¦Æ®³ëÁñ ¿¬¼Ò±âÀÇ À¯µ¿Æ¯¼º

Fludic Characteristics of Precessing Jet Nozzle Combustor

ÀÌÇý¿µ, ÇãȯÀÏ

2007. 08.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 11±Ç 4È£ pp.1~9

 

ÃʼÒÇü ³ëÁñ À¯µ¿Àå¿¡ °üÇÑ ¼öÄ¡Àû ¿¬±¸

A Computational Study on the Characteristics of Flowfields in micro Nozzles

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2007. 12.

Çѱ¹Àü»êÀ¯Ã¼°øÇÐȸÁö Á¦ 12±Ç 4È£ pp.38~43

 

³Ã°¡½º ÃßÁøÀåÄ¡¸¦ ÀÌ¿ëÇÑ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ ¼º´ÉÆò°¡

Performance Evaluation of Micro-nozzle Using cold Gas Propulsion System

Á¤¼ºÃ¶, ±è¿¬È£, ¿ÀÈ­¿µ, ÇãȯÀÏ, ¸í³ë½Å

2007. 12.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 11±Ç 6È£ pp.42~49

 

¾×ü ·ÎÄÏ¿£Áø¿¡¼­ ¼±Çü ¿¬¼Ò ¾ÈÁ¤ÇÑ°è¿¡ ¹ÌÄ¡´Â À¯ÇÑÈ­ÇйÝÀÀ ¹× ¸·³Ã°¢ È¿°ú

Effects of Finite-Rate Chemistry and Film Cooling on Linear Combustion-Stability limit in Liquid rocket Engines

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2006. 02.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 34±Ç 2È£ pp.75~81

 

¸¶ÀÌÅ©·Î ³ëÁñ ¼º´É Æò°¡

Performance test of micronozzle

¹®¼ºÈ¯, ¿ÀÈ­¿µ, ÇãȯÀÏ

2005. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 33±Ç 5È£ pp.72~78

 

LPG ¾×»óºÐ»ç ¿£Áø¿¡¼­ ¾Æ¼¼Åæ PLIF¸¦ ÀÌ¿ëÇÑ ¿¬·áºÐÆ÷ ÃøÁ¤±â¹ý ¿¬±¸

Acetone PLIF for Fuel Distribution measurements in Liquid Phase LPG Injection Engine

¹Ú½ÂÀç, ÇãȯÀÏ, ¿À½Â¹¬, °­°Ç¿ë, ¹èÃæ½Ä

2004. 01.

Çѱ¹ÀÚµ¿Â÷°øÇÐȸ Á¦ 12±Ç 1È£ pp.74~82

 

¸¶ÀÌÅ©·Î ÄÝµå °¡½º Ã߷±âÀÇ ¼±Çà ¿¬±¸

Preliminary Study of Micro Cold Gas Thruster

¹®¼ºÈ¯, ¿ÀÈ­¿µ, ÇãȯÀÏ

2004. 04.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 8±Ç 2È£ pp.54~61

 

¼ÒÇü ¾×ü ÃßÁø±â°ü ¿¬¼Ò ½ÃÇèÀ» À§ÇÑ Ãß·Â ÃøÁ¤ ÀåÄ¡ÀÇ ¼º´É Ư¼º ¿¬±¸

Perfomance Characteristics of Thrust measurement System for Hot-Firing Test of small Liquid Propulsion Engines

±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö, Àå±â¿ø, ÀÌÀç¿ø

2004. 09.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 9È£ pp.122~129

 

¾×ü ·ÎÄÏ¿£ÁøÀÇ ¿¬¼Ò ºÒ¾ÈÁ¤¼º ¿¬±¸ µ¿Çâ

Combustion Instability of Liquid Rocket Engines

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2004. 09.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 9È£ pp.153~161

 

¾×ü ·ÎÄÏ¿£Áø¿¡¼­ ¼±Çü ¿¬¼Ò ºÒ¾ÈÁ¤ Çؼ®À» ÀÌ¿ëÇÑ ¿¬¼Ò ¾ÈÁ¤ÇÑ°è °î¼± °è»ê

Calculation of Comnustion Stability Limits Using Linear Stability Analysis in Liquid Rocket Engines

¼ÕäÈÆ, ¹®À±¿Ï, ÇãȯÀÏ

2004. 10.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 32±Ç 10È£ pp.93~101

 

Àú±Ëµµ À§¼ºÀÇ ÃßÁøÁ¦ ¼Ò¸ðÀ² °èÃø¿¡ °üÇÑ °íÂû

An investigation on the Propellant Comsumption Rate gauged from the low-Earth-orbit Spacecraft

±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö

2003. 01.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 1È£ pp.113~119

 

ÃÊÀ½¼Ó ¿¬¼Ò±â ³»ºÎÀÇ Ãß·Â ºÐÆ÷ °è»êÃÊÀ½¼Ó ¿¬¼Ò±â ³»ºÎÀÇ Ãß·Â ºÐÆ÷ °è»ê

Determination of Thrust Distribution in the Supersonic Combustor

ÇãȯÀÏ

2003. 04.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 4È£ pp.69~75

 

ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·Â ÃøÁ¤ ¹æ¹ý ºñ±³

Comparison of thrust measurement of a supersonic Wind Tunnel

±èÇü¹Î, ÇãȯÀÏ

2003. 05.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 31±Ç Á¦ 5È£ pp.93~99

 

±ØÃÊÀ½¼Ó ÃßÁø±â°ü ¿¬±¸¸¦ À§ÇÑ 2Â÷¿ø ÃÊÀ½¼Ó dzµ¿ ¼³°è ¹× Á¦ÀÛ

Development of a 2-D Supersonic Wind Tunnel for Hypersonic Propulsion Study

±èÁ¤¿ë, ±èÇü¹Î, ÇãȯÀÏ

2003.

»ê¾÷±â¼ú¿¬±¸¼Ò ³í¹®Áý Á¦ 18±Ç Á¦ 1È£ pp.49~56

 

Numerical study of Mixing Enhancement Shock Waves in Model Scramjet Engine

Jiho Kim, Youngbin Yoon, Hwanil Huh, Jeonyeol Choi

2003. 06.

AIAA Journal Vol.41 No.6 pp.1074~1080

https://doi.org/10.2514/2.2047

 

¾×ü·ÎÄÏ¿£Áø °íÁÖÆÄ ¿¬¼ÒºÒ¾ÈÁ¤ÀÇ ¿¹Ãø

Prediction of High Frequency Combustion Instabilities of a Liquid Rocket Engine

À±¿õ¼·, ÇãȯÀÏ

2003. 06.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 7±Ç 3È£ pp.61~68

 

¿ìÁÖºñÇàü ÃßÁø½Ã½ºÅÛ È­ÇÐ½Ä Ã߷±âÀÇ °³¹ß ÇöȲ

Development Status of Chemical Thruster Equipped on Space Vehicle Propulsion System

±èÁ¤¼ö, ±èÀÎÅÂ, ÇãȯÀÏ

2003. 08.

Çѱ¹ÃßÁø°øÇÐȸÁö Á¦ 7±Ç 4È£ pp.80~89

 

Application of Low NOx Combustion Method to Regenerative Oxygen Enriched Combustor

Huh, H(ÇãȯÀÏ), Seo, J.W.(¼­Á¤¿ø), Noh, D.S.(³ëµ¿¼ø)

2002. 06.

Twenty-Ninth International Symposium on Combustion

 

Two Color PIV ±â¹ýÀ» ÀÌ¿ëÇÑ ·¥Á¦Æ®¿£Áø ¿¬¼Ò±â Ư¼º¿¡ ´ëÇÑ ¿¬±¸

A Study on the Characteristics of the Ramjet Engine Combustor using a Two color PIV Technique

¾È±Ôº¹, À±¿µºó, Á¤Àμ®, ÇãȯÀÏ

2002. 01.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 30±Ç 1È£ pp.95~104

 

ÇÏÀ̺긮µå ·ÎÄÏÀÇ °³³ä ¼Ò°³ ¹× ¿¬±¸°³¹ß µ¿Ç⠺м® ¥± - ´ëÇÐ ¹× ¾Æ¸¶Ãß¾î

Recent Progress in Research and Development of Hybrid Rocket:PART ¥±. Research activities of University and Amateurs

±Ç¹ÎÂù, ÇãȯÀÏ

2002. 03.

Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö Á¦ 30±Ç 3È£ pp.155~163

 

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Recent Progress in Research and Development of Hybrid Rocket:PART ¥° International Development Programs of Hybrid Rocket

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2002. 03.

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Spray Characteristics and Exhaust Emission Tests for a Diesel Engine Using Emulsified Fuels

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2002. 04.

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Combustion Efficiencies of Supersonic Flames

Albert Ratner, James F. Driscoll, Hwanil Huh, Rodney A

2001. 03.

Journal of Propulsion and Power Vol. 17 No.2 pp.301~307

https://doi.org/10.2514/2.5742

 

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Micro Propulsion System

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2001. 06.

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Numerical Study on Mixing Enhancement by Shock Waves in a Model SCRamjet Engine

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2000. 01.

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Measured Effect of Shock Wave on the Stability Limits of Supersonic hydrogen-Air Flames

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1999. 02.

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An Experimental Study of Shock Wave Effects on the Model SCRamjet Combustor

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1999. 02.

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Effects of Shock Waves on a Supersonic Hydrogen-Air Jet Flame in a Model SCRamjet Combustor

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1999. 03.

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Measured Supersonic Flame Properties: Heat-Release Patterns, Pressure Losses, Thermal Choking Limits

Yoon, Y., Donbar, U.M., Huh, H., Droscoll, J.F.

1996. 01.

AIAA, Journal of Propulsion and Power, 12, pp. 718~723

https://doi.org/10.2514/3.24093

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