sub menu
gadget
[ ½ÇÇè½Ç ¾È³» ]
´ëÀü±¤¿ª½Ã À¯¼º±¸ ´ëÇзΠ99
Ãæ³²´ëÇб³ Ç×°ø¿ìÁÖ°øÇаú
(°ø´ë 3È£°ü 233È£)
'°í¼ÓÃßÁø ¹× ¿¬¼Ò ½ÇÇè½Ç'
Phone / 042 - 821 - 7771
FAX / 042 - 825 - 9225
ã¾Æ¿À½Ã´Â ±æ
3 tonf±Þ ¾×ü·ÎÄÏ¿£Áø¿ë Àü±âÆßÇÁ ¼ö·ù½ÃÇè
Performance Test of a 3 tonf Class ElecPump for a Liquid Rocket Engine
Á¤¹Î±Ô, °ûÇö´ö, ÇãȯÀÏ
2024. 12.
2024 Çѱ¹À¯Ã¼±â°èÇÐȸ µ¿°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬÀ» Àû¿ëÇÑ 3 tonf±Þ »ó´Ü ¿£Áø ±âÃÊÇؼ®
Basic Analysis of a 3 tonf Class Upper Stage Engine Using an Electric Pump-Fed Cycle
Á¤¹Î±Ô, ¼ÕÁßÈÆ, ÇãȯÀÏ
2024. 10.
2024³âµµ Ç×°ø¿ìÁֽýºÅÛ°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Research Trends in Electric Pump-fed Cycle Engines from 2020 to 2024
, Junghun Son, Mingyu Jeong, Minseo Kim, Seongjun Woo, Hwanil Huh
2024. 10
Asia-Pacific International Symposium on Aerospace Technology 202 4
Heat Transfer Characteristics of Regenerative Cooling for an ED Nozzle Pintle
Changjong Lee, Jeonghang Lee,Hwanil Huh
2024. 10
Asia-Pacific International Symposium on Aerospace Technology 202 4
Chanllenges in Improving Upper Stage Engines: Methane, ED Nozzle, and Electric Pump-fed Cycle
Hwanil Huh, Junghun Son, Jeonghang Lee, Mingyu Jeong, Changjong Lee, Junsub Choi
2024. 07
Conference Proceedings Europe-Korea Conference on Science and Technology 2024
A study on the performance of lithium-ion batteries according to altitude
Minho Lee, Changjong Lee, Jeonghang Lee, Hwanil Huh
2024. 07
Conference Proceedings Europe-Korea Conference on Science and Technology 2024
¼ÒÇü¹ß»çü »ó´ÜÀÇ »çÀÌŬ ¹× ED ³ëÁñ Àû¿ë¿¡ µû¸¥ ¼º´É ºÐ¼® ¿¬±¸
Performance analysis of the Upper Stage of a Small Launch Vehicle with engine cycle and ED nozzle
Çϵ¿ÈÖ, ³ëżº, ÀÌÇüÁø, ÇãȯÀÏ
2024. 06
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
ÇÉƲ ÃÖ¼Ò °Å¸®¿¡ µû¸¥ ED ³ëÁñÀÇ ¼º´É ¹× °ø·ÂÇÏÁß ¼öÄ¡Çؼ®
Numerical Analysis of Performance and Aerodynamic Load According to the Minimum Pintle Distance of ED Nozzle
ÀÌÁ¤Ç×, ÀÌâÁ¾, ±è¹Î¼, ÃÖÁؼ·, ÇãȯÀÏ
2024. 06.
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
°íµµ¿Í ¼¿ ¹è¿¿¡ µû¸¥ ¸®Æ¬ÀÌ¿Â ¹èÅ͸®ÀÇ ³Ã°¢¼º´É
Cooling performance of lithium-ion batteries according to altitude and cell arrangement
ÀÌâÁ¾, ÀÌÁ¤Ç×, ¿ì¼ºÁØ, À̹ÎÈ£, ÇãȯÀÏ
2024. 06
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¿£ÁøÀÇ ¿¬±¸ ¹× °³¹ß µ¿Çâ
Research and Development Trends in Electric Pump-fed Cycle Engines
¼ÕÁßÈÆ, Á¤¹Î±Ô, ±è¹Î¼, ¿ì¼ºÁØ, ÇãȯÀÏ
2024. 06
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
¸®Æ¬ ÀÌ¿Â ¹èÅ͸®ÀÇ ¾Ð·Â º¯È¿¡ µû¸¥ ¼º´É Æò°¡
Performance Evaluation of Lithium-ion Batteries under Pressure Variations
À̹ÎÈ£, ÀÌâÁ¾, ÀÌÁ¤Ç×, ÇãȯÀÏ
2024. 05
2024³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
ED³ëÁñÀÇ ÃµÀÌ Æ¯¼º¿¡ °üÇÑ ±âÃÊ ½ÇÇè
Preliminary Experiment on Transition Characteristics of Expansion Deflection(ED) Nozzle
ÃÖÁؼ·, ÇãȯÀÏ
2024. 05.
2024³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬÀ» Àû¿ëÇÑ »ó´Ü ¿£Áø ±âÃÊÇؼ®
Basic Analysis of Upper Stage Engine Using Electric Pump-Fed Cycle
Á¤¹Î±Ô, ¼ÕÁßÈÆ, ÇãȯÀÏ
2024. 05.
2024³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
ED ³ëÁñ ÇÉƲ ³Ã°¢À¯·Î ¸ð»ç ¼ö·ù½ÃÇèÀåÄ¡ ¼³°è
Design of Test Rig for Simulating Cold Flow in ED Nozzle Pintle Cooling Channel
ÀÌâÁ¾, ÀÌÁ¤Ç×, ÃÖÁؼ· ÇãȯÀÏ
2024. 05.
2024³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
ÇÉƲ ·Îµå ¹ÝÁö¸§¿¡ µû¸¥ ED ³ëÁñÀÇ Ãß·Â ¹× °ø·ÂÇÏÁß ¼öÄ¡Çؼ®
Numerical Analysis of Thrust and Aerodynamic Load of ED Nozzle According to Pintle Rod Radius
ÀÌÁ¤Ç×, ÀÌâÁ¾, ÃÖÁؼ·, ÇãȯÀÏ
2024. 05.
2024³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Applicability of an Electric Pump-fed Cycle Engine for Satellite Thruster
Junghun Son, Mingyu Jeong, Hwanil Huh
2024. 05.
Space Propulsion Conference 2024
Àü±âÆßÇÁ »çÀÌŬ ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ¸ð»ç ±âÃʼö·ù½ÃÇè ¿¹ºñ °á°ú
Preliminary Results of Basic Water Flow Test for Electric Pump-Fed Cycle Supply System Simulation
Á¤¹Î±Ô, ¼ÕÁßÈÆ, ÇãȯÀÏ
2024. 04.
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¿£Áø ±â¹Ý ÀÌ¿øÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ¸ð»ç ¼ö·ù½ÃÇè ¿¹ºñ °á°ú
Preliminary Results of Basic Water Flow Test Simulating Bipropellant Feeding Systems based on Electric Pump-fed Cycle Engines
¼ÕÁßÈÆ, Á¤¹Î±Ô, ÇãȯÀÏ
2024. 04.
2024³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ÀÌ¿øÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ¸ð»ç ¼ö·ù½ÃÇèÀåÄ¡ ±¸Ãà
Construction of Water Flow Test Apparatus to Simulate Bipropellant Supply System in Electric Pump-Fed Cycle
Á¤¹Î±Ô, ¼ÕÁßÈÆ, ÇãȯÀÏ
2023. 11.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
ED ³ëÁñ ÇÉƲÀÇ À¯Ã¼-±¸Á¶ ¿¬¼º Çؼ®À» À§ÇÑ ¿¹ºñ ¿¬±¸
Preliminary Study for Fluid-Structure Interaction Analysis of an ED Nozzle Pintle
ÀÌÁ¤Ç×, ÀÌâÁ¾, ÃÖÁؼ·, ÇãȯÀÏ
2023. 11.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
ED ³ëÁñ ÇÉƲÀÇ ³Ã°¢Ã¤³Î ¼³°è
Design of Regenerative Cooling Channels for ED Nozzle Pintle
ÀÌâÁ¾, ÀÌÁ¤Ç×, ÃÖÁؼ·, ÇãȯÀÏ
2023. 11.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
1-D ½Ã¹Ä·¹À̼ÇÀ» ÀÌ¿ëÇÑ Àü±âÆßÇÁ »çÀÌŬ ¿£ÁøÀÇ ½Ãµ¿ ½Ã ¼ö°ÝÇö»ó Àú°¨ ¿¬±¸
A Study on Reducing Water Hammer during Startup of an Electric Pump-fed Cycle Engine using 1-D Simulation
¼ÕÁßÈÆ, Á¤¹Î±Ô, ÇãȯÀÏ
2023. 11.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
´ÙÃþ¹Ú¸·´Ü¿ÀçÀÇ À¯È¿¹æ»çÀ² ÃßÁ¤ ½ÇÇè Á¶°ÇÀÇ À¯È¿¼º °ËÁõ
Validation of Experimental Conditions for Estimating Effective Emissivity of Multilayer Insulation
±èÁØ°â, *, ÇãȯÀÏ
2023. 11.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Àç»ý³Ã°¢Ã¤³Î ¸ð»ç ȯ°æ ³» ¾×ü ¼ö¼Ò ¿Àü´Þ Ư¼º¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸
Experimental Study on the Heat Transfer Characteristics of Liquid Hydrogen in Simulation of Regenerative Cooling Channel
Çϵ¿ÈÖ, ³ëżº, ÀÌÇüÁø, ÇãȯÀÏ
2023. 11.
2023³âµµ Ç×°ø¿ìÁֽýºÅÛ°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Preliminary Design of an Electric Pump-Fed Cycle for a Methane Upper Stage Engine Based on a 1-D Simulation Analysis
Mingyu Jeong, Junghun Son, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
Analysis of Cooling Performance according to the Thickness of the Pintle Outer Wall
Changjong Lee, Jeonghang Lee, Junsub Choi, Joomi Lee, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
Analysis of flow change before and after transition of ED nozzle
Junsub Choi, Joomi Lee, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
Construction of a Bipropellant Water Flow Test Apparatus Applied with an Electric Pump-fed Cycle
Junghun Son, Mingyu Jeong, Minho Lee, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
Development of Vacuum Facility for evaluating Battery Discharge Characteristics in High Altitude Environments
Minho Lee, Jungyeom Kim, Sangheon Jeong, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
Analysis of the Structural Effect of Aerodynamic Loads on the ED Nozzle Pintle
Jeonghang Lee, Changjong Lee, Joomi Lee, Junsub Choi, Hwanil Huh
2023. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2023
¸Þź ¿¬·á »ó´Ü ¿£Áø ½Ã½ºÅÛ °³¼±À» À§ÇÑ Çٽɱâ¼ú
Core Technologies for Improvement of Methane Upper Stage Engine Systems
ÇãȯÀÏ, ³ëżº, ±èµµ°æ, ÀÌÇüÁø
2023. 07.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
1D ½Ã¹Ä·¹À̼ÇÀ» ÅëÇÑ ED ³ëÁñÀÇ ÇÉƲ ¿Çؼ®
Thermal Analysis of Pintle in ED Nozzle using 1D Simulation
ÀÌâÁ¾, ÀÌÁ¤Ç×, ÃÖÁؼ·, ÀÌÁÖ¹Ì, ÇãȯÀÏ
2023. 06.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ±â¹Ý ÀÌ¿øÃßÁøÁ¦ ¸ð»ç ¼ö·ù½ÃÇèÀåÄ¡ ¼³°è
Design of Bipropellant Water Flow Test Apparatus for Electric Pump-fed Cycle Application
¼ÕÁßÈÆ, Á¤¹Î±Ô, À̹ÎÈ£, ÇãȯÀÏ
2023. 06.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
¿ìÁֹ߻çü »ó´Ü ¿£ÁøÀÇ ±¸Á¶ºñ °³¼±À» À§ÇÑ ED ³ëÁñ Àû¿ë °¡´É¼º °ËÅä
Feasibility Study on the Applicability of an ED Nozzle for Improving Inert Mass Ratio of an Upper Stage Engine in Space Launch Vehicles
ÀÌÁ¤Ç×, ÀÌâÁ¾, ÃÖÁؼ·, ÀÌÁÖ¹Ì, ÇãȯÀÏ
2023. 06.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
»ó´Ü ¿£Áø Àü±âÆßÇÁ »çÀÌŬ Àû¿ëÀ» À§ÇÑ ÃßÁøÁ¦ °ø±Þ ½Ã½ºÅÛ ±â¼ú ¿¬±¸
Research on Propellant Supply System for an Application of Electric Pump-Fed Cycle in an Upper Stage Engine
Á¤¹Î±Ô, ±è°Ç¿µ, ¼ÕÁßÈÆ, À̹ÎÈ£, ÀÌÇüÁø, ÇãȯÀÏ
2023. 06.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
Àç»ý³Ã°¢ ¸ð»ç ȯ°æ ³» ±ØÀú¿Â ÃßÁøÁ¦ÀÇ ¿Àü´Þ Ư¼º¿¡ °üÇÑ ½ÇÇèÀû ¿¬±¸
An Experimental Study on the Heat Transfer Characteristics of Cryogenic Propellants in Regenerative Cooling Channels
Çϵ¿ÈÖ, ³ëżº, ÀÌÇüÁø, ÇãȯÀÏ
2023. 06.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ ¿ìÁÖÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ¿ë ¸®Æ¬ ÀÌ¿Â ¹èÅ͸®ÀÇ ¹æÀü Ư¼º ¿¬±¸
A Study on Discharge Characteristics of Lithium-Ion Batteries for Electric Pump Cycle
À̹ÎÈ£, ÇãȯÀÏ
2023. 05.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¸Þź¿¬·á »ó´Ü Àü±âÆßÇÁ »çÀÌŬ ¿£ÁøÀÇ 1-D ½Ã¹Ä·¹ÀÌ¼Ç Çؼ®
1-D Simulation Analysis of an Electric Pump-Fed Cycle for a Methane Upper Stage Engine
Á¤¹Î±Ô, ¼ÕÁßÈÆ, ÀÌÇüÁø, ÇãȯÀÏ
2023. 05.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
ED ³ëÁñ ÇÉƲÀÇ °ø·ÂÇÏÁß ¼öÄ¡Çؼ®
Numerical Analysis of Aerodynamic Loads on ED Nozzle Pintle
ÀÌÁ¤Ç×, ÀÌâÁ¾, ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ
2023. 05.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¸Þź¿¬·á E-D ³ëÁñÀÇ ÇÉƲ ³Ã°¢ ±âÃʼ³°è¸¦ À§ÇÑ ´ë·ù¿Àü´Þ°è¼ö
Convective Heat Transfer Coefficient for the Basic Design of Pintle Cooling of E-D Nozzle using Methane Fuel
ÀÌâÁ¾, ÀÌÁ¤Ç×, ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ
2023. 05.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¿£ÁøÀÇ Ãß·Â Á¶ÀýÀ» À§ÇÑ ¸ðÅÍ Á¦¾î ¿¹ºñ ½ÇÇè
Preliminary Experiments on Motor Control for Thrust Control of an Electric Pump-fed Cycle Engine
¼ÕÁßÈÆ, Á¤¹Î±Ô, À̹ÎÈ£, ÀÌÇüÁø, ÇãȯÀÏ
2023. 05.
2023³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¾×ü·ÎÄÏ¿£Áø Ãß·Â Á¦¾î¸¦ À§ÇÑ ÃßÁøÁ¦ °ø±Þ°è M&S
Propellant Supply System M&S for Thrust Control of Electric-Pump-Fed Cycle Liquid Rocket Engines
±èÇýÀÎ, ±è°Ç¿µ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2023. 05.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
500N±Þ ÃʼÒÇü Expansion-Deflection ³ëÁñ ¼³°è
Lab-Scale Expansion-Deflection Nozzle Design for 500N
ÇÑ°æȯ, Çϵ¿ÈÖ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2023. 05.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¹× E-D ³ëÁñÀ» Àû¿ëÇÑ ¼ÒÇü ¹ß»çü ¼º´É ºÐ¼®
Performance Analysis of Small Launch vehicle with Electric Pump Cycle and E-D Nozzle
Çϵ¿ÈÖ, ÇÑ°æȯ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2023. 05.
2023³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Environmental Test of Lithium-ion Batteries for Electric Pump-fed Systems Applications
Minho Lee, Junghun Son, Jeonghang Lee, Hwanil Huh
2023. 03.
11th Asian Joint Conference on Propulsion and Power 2023
Battery Mass Estimation of an Electric Pump Cycle for Upper-Stage Propulsion Systems
Jungyeom Kim, Geon Young Kim, Minho Lee, Mingyu Jeong, Hwanil Huh, Hyoung Jin Lee
2023. 03.
11th Asian Joint Conference on Propulsion and Power 2023
Ansys Fluent¸¦ È°¿ëÇÑ Àü±âÆßÇÁ »çÀÌŬ¿ë ¸®Æ¬ÀÌ¿Â ¹èÅ͸®ÀÇ ¾ÈÀü¼º °ËÅä
Safety Review of a Li-ion Battery for Electric Pump Cycle Applications with Ansys Fluent
À̹ÎÈ£, ¼ÕÁßÈÆ, ÀÌÁ¤Ç×, ±èÁØ°â, ÇãȯÀÏ
2022. 11.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
¼ÒÇü ¾×ü·ÎÄÏ¿£ÁøÀÇ ÆßÇÁ Á¦ÀÛ ¹× µ¿Àû Ư¼º ¿¬±¸
A Study on the Pump Manufacturing and Dynamic Characteristic of Small Liquid Rocket Engines
±èÇýÀÎ, ¼ÁöÈñ, Çϵ¿ÈÖ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2022. 11.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
¿ìÁֹ߻çüÀÇ »ó´Ü ¿£Áø °³¹ß µ¿Çâ
Trend in Upper Stage Engine Development of Space Launch Vehicles
ÇÑ°æȯ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2022. 11.
2022³âµµ Ç×°ø¿ìÁֽýºÅÛ°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Simulation Study of an Electric Pump-fed Cycle Flow Characteristics by Using a 1-D Modeling Analysis
Geon Young Kim, Hyoung Jin Lee, Hwanil Huh
2022. 10.
Asia-Pacific International Symposium on Aerospace Technology 2022
Evaluation of a Space-borne MLI Performance by Using an Experimental Estimation
Geon Young Kim, *, Jungyeom Kim, Hwanil Huh
2022. 06.
32nd International Symposium on Rarefied Gas Dynamics
Experimental Estimation of the Effective Emissivity of a Space-borne MLI Based on Design Parameters
Geon Young Kim, *, Jungyeom Kim, Hwanil Huh
2022. 07
9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)
Thrust Analysis by Length Reduction of an ED Nozzle with Fixed Expansion Ratio
Joomi Lee, Junsub Choi, Hwanil Huh
2022. 07.
9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)
Mass Estimation of an Electric Pump Cycle Engine for 30kN-class Upper Stage Launch Vehicle Based on a Battery Technology
Jungyem Kim, Geon Young Kim, Hyoung Jin Lee, Hwanil Huh
2022. 07.
9th European Conference for Aeronautics and Space Sciences(EUCASS 2022)
¾×ü ÃßÁø±â°ü¿ë Àü±âÆßÇÁ »çÀÌŬ ¸ð»ç ¼ö·ù½ÃÇèÀåÄ¡ÀÇ ÆßÇÁ ȸÀü¼ö Á¦¾îÀåÄ¡ ±¸Ãà
Pump RPM Control System of a Water Flow Test Equipment Simulating an Electric Pump-fed Cycle of a Liquid Propulsion System
±è°Ç¿µ, ÀÌÇüÁø, ÇãȯÀÏ
2022. 06.
2022³âµµ ±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý
¾×ü·ÎÄÏ °ø±Þ ½Ã½ºÅÛÀÇ µ¿Àû ¸ðµ¨¸µ ¹× ½Ã¹Ä·¹ÀÌ¼Ç °ËÁõ
Dynamic Modeling and Simulation Validation of a Liquid Rocket Supply System
±èÇýÀÎ, ±è°Ç¿µ, ³ëżº, ÇãȯÀÏ, ÀÌÇüÁø
2022. 05.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬÀ» Àû¿ëÇÑ ¹ß»çü »ó´ÜÀÇ Áß·®ÀÌµæ ¿¹Ãø
Mass Analysis of Electric Pump Cycle Engine according to Combustion Chamber Pressure and Burning Time
±èÁØ°â, ±è°Ç¿µ, ÀÌÇüÁø, ÇãȯÀÏ
2022. 05.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
E-D ³ëÁñÀÇ ÇÉƲ Çü»ó¿¡ µû¸¥ Ã߷°ú °ø·ÂÇÏÁß ºÐ¼®
Thrust and Aerodynamic Load Analysis according to the Pintle Shape of the E-D Nozzle
ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ
2022. 05.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ÃßÁø ÀåÄ¡ÀÇ °ø±Þ°è À¯·® Á¦¾î ½Ã½ºÅÛ ±âÃÊ ¿¬±¸
Preliminary Study on a Flow Control System of an Electric Pump-fed Cycle
±è°Ç¿µ, ±èÁØ°â, À̹ÎÈ£, ÀÌÇüÁø, ÇãȯÀÏ
2022. 05.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¿ìÁÖ¿ë ¹èÅ͸®ÀÇ ±¹¿Ü ¿ìÁÖ È¯°æ ½ÇÇè
Overseas Space Environment Tests of Space-borne Batteries
À̹ÎÈ£, ±è°Ç¿µ, ÇãȯÀÏ
2022. 05.
2022³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
³ëÁñ ¾Ð·Âºñ¿¡ µû¸¥ E-D ³ëÁñÀÇ Á¤»ó»óÅ ¼öÄ¡Çؼ®
Steady-state Numerical Analysis of an Expansion-Deflection Nozzle According to Nozzle Pressure Ratios
ÃÖÁؼ·, ÇãȯÀÏ
2021. 11.
2021³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ·ÎÄÏ ¿£ÁøÀÇ ÆßÇÁ ȸÀü¼ö º¯È¿¡ µû¸¥ À¯µ¿ Ư¼º ÆľÇ
Flow Characteristics Identification of an Electric Pump-fed Cycle according to Pump RPM Control
±è°Ç¿µ, ±èÁØ°â, ÀÌÇüÁø, ÇãȯÀÏ
2021. 11.
2021³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
ÇÉƲ º¯°î °¢µµ°¡ °íÁ¤µÈ 500N±Þ E-D ³ëÁñÀÇ Æ¯¼º
Characteristics of an 500N E-D Nozzle with a Fixed Pintle Inflection Angle
ÀÌÁÖ¹Ì, ÃÖÁؼ·, ÇãȯÀÏ
2021. 11.
2021³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
¿ìÁÖ¿ë ´ÙÃþ¹Ú¸·´Ü¿ÀçÀÇ À¯È¿¹æ»çÀ² ÃßÁ¤°á°ú °ËÅä II
Review on Estimation Result of Effective Emissivity of Space-borne MLI II
ÀåÁø¼ö, ±è°Ç¿µ, ÇãȯÀÏ
2021. 11.
2021³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
Components Design of an Experimental System for a Lab-Scaled Electric Pump-fed Cycle
Geon Young Kim, Hyoung Jin Lee, Hwanil Huh
2021. 11.
Asia-Pacific International Symposium on Aerospace Technology 2021
¼ÒÇü ¾×ü·ÎÄÏ °ø±Þ°èÀÇ Àúºñ¼Óµµ ¿ø½ÉÆßÇÁ ¼³°è ¿¬±¸
A Study on the Design of Centrifugal Pump with Low Specific Speed for a Propellant Supply System of Small Liquid Rocket
±èÇýÀÎ, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø
2021. 11.
2021³âµµ ±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý
¾×ü·ÎÄÏ ¿£Áø¿ë Àü±âÆßÇÁ »çÀÌŬ ¸ðµ¨¸µ ¹× ¸ðÅÍ ¿ä±¸ ¼º´É ÆľÇ
Modeling of an Electric Pump-fed Cycle for a Liquid Rocket Engine and Identification of Motor Requirement
±è°Ç¿µ, ±â¿ø±Ù, ÇãȯÀÏ
2021. 11.
2021³âµµ ±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý
Study on Numerical Evaluation Method for Cooling Capability of Thermo-Electric Cooler and Effectiveness Assessment of CAE Simulation by using Simplified Thermal Boundary Conditions
* , Hwanil Huh
2021. 08.
50th International Conference on Environmental Systems
¼ÒÇü ¾×ü·ÎÄÏ¿£Áø¿ë Àúºñ¼Óµµ ÆßÇÁ ¼³°è
Design of a Low Specific Speed Pump for Small Liquid Rocket Engines
±èÇýÀÎ, ÇãȯÀÏ, ÀÌÇüÁø
2021. 04.
2021³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¿ìÁÖ¿ë ´ÙÃþ¹Ú¸· ´Ü¿ÀçÀÇ À¯È¿ ¹æ»çÀ² ÃßÁ¤À» À§ÇÑ ÃøÁ¤ ½Ã½ºÅÛ ±¸Ãà
Development of Measurement System for Estimation of Effective Emissivity of Space-borne MLI
* , ÃÖÁؼ·, ÇãȯÀÏ, Á¤»óÇå
2021. 04.
2021³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¿ìÁÖ¿ë ´ÙÃþ¹Ú¸·´Ü¿ÀçÀÇ À¯È¿¹æ»çÀ² ÃßÁ¤°á°ú °ËÅä
Review on Estimation Result of Effective Emissivity of Space-borne MLI
* , ±è°Ç¿µ, ÇãȯÀÏ
2021. 04.
2021³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Àü±âÆßÇÁ »çÀÌŬ ¸ð»ç ¼ö·ù½ÃÇèÀåÄ¡ Á¤Æ¯¼º ¸ðµ¨¸µ ¹× ¸ðÅÍ È¸Àü¼ö¿¡ µû¸¥ Â÷¾Ð ¿¹Ãø
Static Modeling of a Water Flow Test Equipment Simulating an Electric Pump Cycle and Estimation of Differential Pressure According to the Motor RPM
±è°Ç¿µ, ÃÖÁؼ·, ÇãȯÀÏ
2021. 04.
2021³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
¼ÒÇü ¾×ü·ÎÄÏ¿£Áø¿ë Àúºñ¼Óµµ ÆßÇÁ ¼³°è
Design of a Low Specific Speed Pump for Small Liquid Rocket Engines
±èÇýÀÎ, ÇãȯÀÏ, ÀÌÇüÁø
2021. 04.
2021³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Performance Analysis of KSLV-II with a Dual Bell Nozzle Using 1-D Simulation
Junsub Choi, Hwanil Huh
2021. 03.
10th Asian Joint Conference on Propulsion and Power 2021
Fundamental Tests of the Propellant Supply System of the Electric-pump Cycle for Space Propulsion Systems
Wonkeun Ki, Jaecheong Lee, Geon Young Kim, Jumi Lee, Hwanil Huh
2021. 03.
10th Asian Joint Conference on Propulsion and Power 2021
¼ÒÇü ¾×ü·ÎÄÏ¿£Áø °ø±Þ°èÀÇ ¼öÇÐÀû ¸ðµ¨¸µ ±â¹ý °ËÁõ
Validation of Medeling Method for the Supply System of Small-sized Liquid Rocket Engine
ÀÌÁÖ¿¬, ±â¿ø±Ù, ÇãȯÀÏ, ³ëżº, ÀÌÇüÁø
2020. 11.
2020³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
¼±¹Ú¿ë °¡½ºÅͺó GE LM2500 ¿£ÁøÀÇ µ¿Àû ½Ã¹Ä·¹À̼Ç
Dynamic Simulation of a GE LM2500 Engine for Marin Applications
¹é°æ¹Ì, ÇãȯÀÏ
2020. 11.
2020³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
±ØÃÊÀ½¼Ó È°°ø ºñÇàü(HGV)ÀÇ ºñÇà½ÃÇè ÇöȲ
Flight Test Status of Hypersonic Glide Vehicles
Ȳ±â¿µ, ÇãȯÀÏ
2020. 11.
2020³âµµ Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
ÇÔÁ¤¿ë °¡½ºÅͺóÀÇ Á¤»ó»óÅ ¼º´ÉÇؼ®
Steady-state Performance Analysis of a Naval Ship Gas Turbine
¹é°æ¹Ì, ÇãȯÀÏ
2020. 11.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý 2020-1997
±ØÃÊÀ½¼Ó ºñÇàü(¹Ì»çÀÏ)ÀÇ °³¹ß µ¿Çâ Á¶»ç
Development Trend Survey of Hypersonic Vehicles (Missiles)
Ȳ±â¿µ, ÇãȯÀÏ
2020. 11.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý 2020-1747
¼ö·ù½ÃÇèÀ» ÅëÇÑ ¾×ü·ÎÄÏ °ø±Þ°è ¸ðµ¨¸µ °ËÁõ
Modeling Validation of Liquid Propellant Supply System through Cold Flow Test
ÀÌÁÖ¿¬, ³ëżº, ÀÌÇüÁø, ±â¿ø±Ù, ÇãȯÀÏ
2020. 11
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý 2020-2037
¼ÒÇü ¾×ü·ÎÄÏ¿ë Àü±âÆßÇÁ »çÀÌŬÀÇ ÃßÁøÁ¦ °ø±Þ ¸ð»ç ¼ö·ù ½ÇÇè ¿¬±¸
Study on Water Flow Test Simulating the Supply of Propellants in Electric Pump Cycle for Small Liquid Rockets
±â¿ø±Ù, ±è°Ç¿µ, Ȳ±â¿µ, ÇãȯÀÏ
2020. 11.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý 2020-1993
MT30 ¿£ÁøÀÇ ¼º´É ¸ðµ¨¸µ¿¡ °üÇÑ ¿¬±¸
A Study on Performance Modeling of MT30 Engine
¹é°æ¹Ì, ±âÀÚ¿µ, ÇãȯÀÏ
2020. 07.
2020³âµµ Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Study on the Effect of Each Design Parameter of Space-borne MLI on the Effective Emissivity
* , Hwanil Huh
2019. 12.
Asia-Pacific International Symposium on Aerospace Technology 2019
¸¶ÇÏ 7 Ãæ°ÝÆÄ Åͳο¡¼ Æ÷½º¼¾¼¸¦ È°¿ëÇÑ Ç×·ÂÃøÁ¤
±âÃʽÇÇè
Fundamental Experiments for Drag Measurement using a Force Sensor in a Mach 7 Shock Tunnel
ÀÌÀçû, ÀÌÀ¯¼®, ÀÌÇüÁø, ÇãȯÀÏ
2019. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2019-2018
¸¶ÇÏ 3.8 Free-jet ŸÀÔ ÃÊÀ½¼Ó dzµ¿ ¼³°è ¹× ±¸Ãà
Design and Construction of the Mach 3.8 Free-jet Type Supersonic Wind Tunnel
ÀÌÀ¯¼®, ±â¿ø±Ù, ÀÌÀçû, ÀÌÇüÁø, ÇãȯÀÏ
2019. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2019-2021
³ëÁñ¸ñ ¿ÜºÎÇü ÇÉƲ ³ëÁñÀ» Àû¿ëÇÑ Çѱ¹Çü¹ß»çüÀÇ
³ëÁñ ±æÀÌ Àý°¨ °¡´É¼º
Possibility of Reducing Nozzle Length for the KSLV-II an External Pintle Nozzle
À̱âȯ, ±èÇѼÖ, ÇãȯÀÏ
2019. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2019-2020
»óÃþÃßÁø½Ã½ºÅÛ¿ë Àü±âÆßÇÁ »çÀÌŬÀÇ ±âÃʽÃÇèÀåÄ¡ ±¸¼º
Fundamental Experimental Setup of an Electric-pump
Cycle for Space Propulsion Systems
±â¿ø±Ù, ÀÌÀçû, ÇãȯÀÏ
2019. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2019-2019
Experimental Investigation on Darg Reduction by Plasma Counterflow Jets in Mach 7 Shock Tunnel
Jaecheong Lee, Yuseok Lee, Yongchan Kim, Hyoungjin Lee, Hwanil Huh
2019. 10.
70th International Astronautical Congress 2019
Preliminary Design of High Speed Test Facility for Counterflow Jet Experiments Reducing Heat and Drag
Yuseok Lee, Hansol Kim, Hwanil Huh
2019. 10.
70th International Astronautical Congress 2019
Quantitative Analysis on the Radiative and Conductive Heat Transfer through Space-Borne MLI Based on Theorectical Approach
* , Seung-Uk Yang, Yong-Sang Jung, Hwanil Huh
2019. 07.
49th International Conference on Environmental Systems
¿ìÁÖ¿ë MLIÀÇ À¯È¿ ¹æ»çÀ² ÃßÁ¤À» À§ÇÑ ¼³°è ¿ä¼Ò ±â¹ÝÀÇ ¼öÄ¡ ¸ðµ¨¸µ ¹× ºÐ¼® ¹æ¾È¿¡ ´ëÇÑ ¿¬±¸
Study on Numerical Modeling and Analysis based on Design Parameters
for the Estimation of Effective Emissivity of Space-borne MLI
* , ÇãȯÀÏ
2019. 05.
Ç×°ø¿ìÁֽýºÅÛ°øÇÐȸ Ãá°èÇмú´ëȸ
¿ìÁÖ¿ë MLIÀÇ À¯È¿ ¹æ»çÀ²¿¡ ´ëÇÑ ÃßÁ¤ ±â¹ý ¹× À¯È¿¼º¿¡ ´ëÇÑ °ËÅä
Study on Estimation Technique and Effectiveness of
the Effective Emissivity of Space-borne MLI
* , ÇãȯÀÏ
2019. 05.
Ç×°ø¿ìÁֽýºÅÛ°øÇÐȸ Ãá°èÇмú´ëȸ
Fundamental Numerical Study for Performance of E-D Rocket Nozzle according to the Pintle Design Parameters
Kihwan Lee, Hansol Kim, Taesoek Moon, Hwanil Huh
2019. 08.
The 10th Asian-Pacific Conference on Aerospace Technology and Science & The 4th Asian joint Symposium on Aerospace Engineering
Parametric Studies of Diffuser for Constant Test Section Mach Number in Free-jet Supersonic Wind Tunnel
Yuseok Lee, Hyoungjin Lee, Hwanil Huh
2019. 08.
The 10th Asian-Pacific Conference on Aerospace Technology and Science & The 4th Asian joint Symposium on Aerospace Engineering
¿ì¸®³ª¶ó ¿ìÁÖ°³¹ß Àü´ãÁ¶Á÷¿¡ ´ëÇÑ Á¦¾ð
À±¿µºó, ÇãȯÀÏ
2019. 05.
±Û·Î¹úÇ×°ø¿ìÁÖ»ê¾÷ÇÐȸ Á¦5ȸ Çмú¼¼¹Ì³ª
A Study of Unsteady Characteristics on Two-axis Pintle Thrusters with the Different Pintle Shape
Jaecheong Lee, Hwanil Huh
2019. 08.
Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019
Design of External Pintle Nozzle with Pintle Injector for Methane Rocket Engine
Hansol Kim, Kihwan Lee, Hwanil Huh
2019. 08.
Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019
Experimental Study on an Expansion-Deflection Nozzle Characteristics according to the Pintle Inflection Angle
Kihwan Lee, Sanghyeon Park, Hwanil Huh
2019. 08.
Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019
Research Trends of Electric-Pump Cycle for Liquid Rocket Engines in Republic of Korea
Wonkeun Ki, Jaecheong Lee, Hwanil Huh
2019. 08.
Conference Proceedings US-Korea Conference on Science, Technology and Enterpreneurship 2019
Fundamental Experiment on Actuators for Two-Axis Pintle Thrusters
Jaecheong Lee, Hwanil Huh
2019. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2019
Characteristics of Supersonic Diffuser with Constant Circular Cross Section
Yuseok Lee, Hwanil Huh
2019. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2019
Fundamental Numerical Study for Performance of an Expansion-Deflection Nozzle according to the Base Nozzle Length
Kihwan Lee, Hansol Kim, Hwanil Huh
2019. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2019
A Numerical Study on the Variation of Internal Flow Field of the External Pintle Nozzle with Pintle Radius
Hansol Kim, Kihwan Lee, Hwanil Huh
2019. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2019
Conceptual Design on Main Components of the Electric-Pump Cycle Engine
Wonkeun Ki, Jaecheong Lee, Hwanil Huh
2019. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2019
¸¶ÇÏ 3.8 Free-jet ŸÀÔ ÃÊÀ½¼Ó dzµ¿ °³³ä ¼³°è
Conceptual Design of a M3.8 Free-jet Type Supersonic Wind Tunnel
ÀÌÀ¯¼®, ÀÌÀçû, ÀÌÇüÁø, ÇãȯÀÏ
2019. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý 2019-1253
ÇÉƲ ¹ÝÁö¸§¿¡ µû¸¥ È®Àå-±¼Àý ·ÎÄÏ ³ëÁñÀÇ ¼º´É¿¡ ´ëÇÑ ±âÃÊ Àü»ê¼öÄ¡Çؼ®
Fundamental Numerical Study for Performance of an E-D Rocket Nozzle according to the Pintle Radius
À̱âȯ, ±èÇѼÖ, ÇãȯÀÏ
2019. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý 2019-1232
¹Ì±¹ÀÇ ¾×ü·ÎÄÏ¿£Áø¿ë Àü±âÆßÇÁ »çÀÌŬ ¿¬±¸ µ¿Çâ
Research Trends of Electric-Pump Cycle for Liquid Rocket Engines in U.S.
±â¿ø±Ù, ÀÌÀçû, ÀÌÀ¯¼®, À̱âȯ, ±èÇѼÖ, ÇãȯÀÏ
2019. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý 2019-1230
ÃÊ°í¼Ó ºñÇàüÀÇ Ç׷°¨¼Ò¸¦ À§ÇÑ ÇöóÁ ºÐ»çÀåÄ¡ °³³ä¼³°è
Conceptual Design on Plasma Counterflow Jets for Drag Reduction of a High Speed Vehicle
ÀÌÀçû, ÀÌÀ¯¼®, ÇãȯÀÏ
2018. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2018-2215
Ãæ³²´ëÇб³ 2-D ÃÊÀ½¼Ó dzµ¿ ½ÃÇèºÎ È®Àå °³¼±À» À§ÇÑ Àü»ê¼öÄ¡Çؼ® ¿¬±¸
Numerical analysis of 2-D Supersonic Wind-tunnel in Chungnam National University for Expanding Test Section
ÀÌÀ¯¼®, ÀÌÀçû, ÀÌÇüÁø, ÇãȯÀÏ
2018. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2018-2203
3D ÇÁ¸°Æà E-D ³ëÁñÀÇ Ç¥¸éÁ¶µµ °³¼± ÈÄ ±âÃÊ ½ÇÇè ¿¬±¸
Fundamental Experimental Study of a 3D Printing E-D Nozzle after Improvement of Surface Roughness
À̱âȯ, ÇãȯÀÏ
2018. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 2018-2161
3D ÇÁ¸°Å͸¦ È°¿ëÇÑ E-D ³ëÁñ °ø¾Ð ½ÇÇè ¿¹ºñ °á°ú
Preliminary Results of E-D Nozzle Pneumatic Experiment using 3D Printer
À̱âȯ, ÀÌÀ¯¼®, ¹Ú»óÇö, ÇãȯÀÏ
2018. 12.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1201-1202
ÇÉƲ ÀÎÁ§Å͸¦ °áÇÕÇÑ ³ëÁñ¸ñ ¿ÜºÎÇü ÇÉƲ ³ëÁñÀÇ °³³ä ¼³°è
Conceptual Design of External Pintle Nozzle with Pintle Injector
±èÇѼÖ, ÀÌÀçû, ÇãȯÀÏ
2018. 12.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1199-1200
Effect of Nozzle Geometry on Counterflow Jets for Drag Reduction of a High Speed Vehicle
Jaecheong Lee, Jongin Choi, Yuseok Lee, Hwanil Huh
2018. 10.
69th International Astronautical Congress 2018
¿Âµµ Áõ°¡¿¡ µû¸¥ Áú·® À¯·® °¨¼Ò°¡ ¿ª ºÐ»ç Á¦Æ®¿¡ ¹ÌÄ¡´Â ¿µÇ⠺м®
Analysis of Effect of the Counterflow jets according to the Reduction of Mass Flow Rate on increases in Temperature
ÀÌÀ¯¼®, À̱âȯ, ÀÌÀçû, ÇãȯÀÏ
2018. 08.
Á¦10ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ
õÀÌ NPR ±¸°£¿¡¼ÀÇ E-D ³ëÁñ À¯µ¿Àå ºÐ¼®
Analysis of E-D Nozzle Flow in Transition Nozzle Pressure Ratios
À̱âȯ, ÃÖÁؼ·, ÇãȯÀÏ
2018. 08.
Á¦10ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ
°íµµ º¸Á¤¿ë µà¾ó º§ ³ëÁñÀÇ ±âÃÊ Àü»ê¼öÄ¡Çؼ®
Basic Numerical Analysis of Altitude-Compensating Dual Bell Nozzles
ÃÖÁؼ·, ÇãȯÀÏ
2018. 08.
Á¦10ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ
³ëÁñ ¸ñ°¢µµ¿¡ µû¸¥ ³ëÁñ¸ñ ¿ÜºÎÇü ÇÉƲ ³ëÁñÀÇ Àü»ê¼öÄ¡Çؼ®À» ÅëÇÑ À¯µ¿ Ư¼º ºÐ¼®
Flow Characteristics through Numerical Analysis of External Pintle Nozzle with Nozzle Throat Angle
±èÇѼÖ, ¹®Å¼®, ÀÌÀçû, ÇãȯÀÏ
2018. 08.
Á¦10ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ
Experiments of Counterflow Jets using Air and Plasma Injection according to Mach Number of Nozzle Exit
Yuseok Lee, Kihwan Lee, Jaecheong Lee, Hwanil Huh
2018. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-05
A Study of Steady Characteristics on Two-Axis Pintle Thrusters with the Different Pintle Shape
Jaecheong Lee, Hwanil Huh
2018. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-04
A Study on Internal Flow Field of External Pintle Nozzle with the Different Nozzle Throat Angle
Hansol Kim, Taeseok Moon, Jaecheong Lee, Hwanil Huh
2018. 08.
Conference Proceedings Europe-Korea Conference on Science and Technology 2018, EKC2018-MA-03
ºÐ»ç ³ëÁñÀÇ Á÷°æ¿¡ µû¸¥ ¿ªºÐ»ç ÀåÄ¡ÀÇ À¯µ¿ Ư¼º ºÐ¼®
Analysis of the Flow Characteristics of the Counterflow Jets according to the Diameter of the Injection Nozzle
ÀÌÀçû, ÀÌÀ¯¼®, ÇãȯÀÏ
2018. 06.
±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.1247-1248
Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ÇÏ´Â ÄɷνŠ·ÎÄÏ ¿£Áø°ú ¸Þź ·ÎÄÏ ¿£ÁøÀÇ ºñÃß·Â ºñ±³
Comparative Study of Specific Impulse Between Kerosene Rocket Engine and Methane Rocket Engine Based on KSLV-II
±èÇѼÖ, ¹®Å¼®, ÀÌÀçû, ÇãȯÀÏ
2018. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.146-147
ÃÊÀ½¼Ó ȯ°æ¿¡¼ ¹ÞÀ½°¢°ú ³ëÁñ Ãⱸ ¼Óµµ¿¡ µû¸¥ ¿ªºÐ»ç Á¦Æ® Ç×·Â ÃøÁ¤ ¿¬±¸
A Study on the Drag Measurement of Counterflow Air Jet with Angle of Attacks and Nozzles Exit Speed under Supersonic Condition
ÀÌÀ¯¼®, À̱âȯ, ÀÌÀçû, ÇãȯÀÏ
2018. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.24-25
±ØÃÊÀ½¼Ó Ãæ°ÝÆÄ Ç³µ¿À» ÀÌ¿ëÇÑ ÇöóÁ ºÐ»çÀåÄ¡ ±âÃÊ ½ÇÇè
EFundamental Experiment on Plasma Counterflow Jets Using Hypersonic Shock Tunnel
ÀÌÀçû, °½Â¿ø, ÃÖÁ¾ÀÎ, ±è¿ëÂù, Â÷½Â¿ø, ÀÌÇüÁø, ÇãȯÀÏ
2018. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.22-23
Analysis of Injection Conditions of Counterflow Jets for Drag Reduction of a High Speed Vehicle
Jaecheong Lee, Jongin Choi, Seungwon Kang, Hwanil Huh.
2018. 03.
2018 the Asian Joint Conference on Propulsion and Power, AJCPP2018-056
ÀÚÀ¯À¯µ¿ Á¶°Ç¿¡ µû¸¥ °ø±â ºÐ»çÀåÄ¡ÀÇ À¯µ¿ Çü»ó¿¡ ´ëÇÑ ±âÃÊ ½ÃÇè ¿¬±¸
Fundamental Tests on the Flow Structure of Air Counterflow Jets in Free Stream Conditions.
ÃÖÁ¾ÀÎ, °½Â¿ø, ÀÌÀçû, ÇãȯÀÏ
2017. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.259-260.
³·Àº ³ëÁñ ¾Ð·Âºñ ±¸°£¿¡¼ÀÇ E-D ³ëÁñ Àü»ê¼öÄ¡Çؼ® ¹× ½ÇÇè ¿¹ºñ °á°ú
Numerical Analysis and Preliminary Experimental Results of E-D Nozzle in Low Nozzle Pressure Ratios
¹Ú»óÇö, ¹®Å¼®, ÇãȯÀÏ
2017. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.71-72.
ÇÉƲ ÃÖ¼Ò °Å¸®¿¡ µû¸¥ E-D ³ëÁñÀÇ ¼º´É ºÐ¼®À» À§ÇÑ ±âÃÊ Àü»ê¼öÄ¡Çؼ®
Basic Numerical Study for Performance Analysis of an E-D nozzle according to the Minimum Distance
¹®Å¼®, ¹Ú»óÇö, ÇãȯÀÏ
2017. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.73-74.
¹°·ÎÄÏ ³ëÁîÄÜ Çü»ó¿¡ µû¸¥ ºñÇà°Å¸® º¯È ºÐ¼®
Analysis of Flight Range for Changes Shape of Water Rocket Nose Cones
±èÇѼÖ, ÇãȯÀÏ
2017. 11
2017 ´ëÇѱâ°èÇÐȸ Ãß°è Á¾ÇÕ Çмú´ëȸ, WISET °á°ú¹ßÇ¥´ëȸ
Evaluation of Payload Gain according to E-D Nozzle Length Reduction
Taeseok Moon, Hwanil Huh
2017. 10.
2017 Aisa-Pacific International Symposium on Aeroapace Technology, APISAT2017-C6-1
Performance Analysis of an Expansion-Deflection Nozzle According to Initial Angle of a Pintle
Taeseok Moon, Sanghyeon Park, Junsub Choi, Hwanil Huh
2017. 07.
Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017
Fundamental Experiments on Temperature Measurements of a Plasma Jet
Jongin Choi, Seungwon Kang, Jaecheong Lee, Hwanil Huh
2017. 07.
Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017
Experimental Study of Flow Characteristics in an Expansion-Deflection Nozzle at Low Nozzle Pressure Ratios
Sanghyeon Park, Taeseok Moon, Junsub Choi, Hwanil Huh
2017. 07.
Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017
Construction of Fundamental Experiment System of a Plasma Generator for Drag Reduction Research
Seungwon Kang, Jongin Choi, Jaecheong Lee, Hwanil Huh
2017. 07.
Conference Proceedings Europe-Korea Conference on Science and Technology 2017, EKC2017
ºÐ»çÀåÄ¡¸¦ ÀÌ¿ëÇÑ ÃÊ°í¼Ó ºñÇàüÀÇ ¿º¸È£ ¹× Ç׷°¨¼Ò¿¡ ´ëÇÑ ÀϺ»ÀÇ ¿¬±¸ µ¿Çâ
Research Trends on Heating and Drag Reduction of High-Speed Vehicles Using Counter-Flow Jets in Japan
ÃÖÁ¾ÀÎ, ÀÌÀçû, °½Â¿ø, ÇãȯÀÏ
2017. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.1111-1112
Ç׷°¨¼Ò¿ë ÇöóÁ ºÐ»ç ÀåÄ¡¸¦ »ç¿ëÇÑ ÃÊ°í¼Ó ºñÇàüÀÇ ¼±µÎºÎ Ç¥¸é ¿Âµµ ÃøÁ¤
Surface Temperature Measurements of a High Speed Vehicle Using Plasma Generator for Drag Reduction Applications
ÀÌÀçû, °½Â¿ø, ÃÖÁ¾ÀÎ, ÇãȯÀÏ
2017. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.1085-1086
Fundamental Research on Altitude Compensating Nozzles
Hwanil Huh
2017. 05.
1st Korea-Russia Science and Technology Day
µà¾ó º§ ³ëÁñ¿¡ È®Àå-±¼Àý(E-D) ³ëÁñ °³³äÀ» Àû¿ëÇÑ ±âÃÊ Àü»ê¼öÄ¡Çؼ®
Numerical Study of Dual Bell Nozzle by applying the Concept of Expansion-Deflection Nozzle
¹®Å¼®, ¹Ú»óÇö, ÃÖÁؼ·, ÇãȯÀÏ
2017. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.679-681
µà¾ó º§ ³ëÁñÀÇ ÃµÀÌƯ¼º¿¡ ´ëÇÑ Á¤»ó»óÅ ¼öÄ¡Çؼ® ¿¬±¸
Numerical investigation of steady state for transition characteristics of dual-bell nozzle
ÃÖÁؼ·, ÇãȯÀÏ
2016. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.85-86
°íµµº¸Á¤¿ë E-D ³ëÁñÀÇ ¼³°è º¯¼ö¿¡ ´ëÇÑ °íÂû
Study of an E-D Nozzle Design Parameters for Altitude Compensation
¹Ú»óÇö, ¹®Å¼®, ÇãȯÀÏ
2016. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ´«¹®Áý pp.1162-1163
ÇöóÁ ºÐ»çÀåÄ¡ ±¸¼º ¹× Ç×·ÂÃøÁ¤ ±âÃÊ ½ÇÇè
The Configuration and Fundamental Test of Plasma Counterflow Jet
ÃÖÁ¾ÀÎ, °½Â¿ø, ÀÌÀçû, ÇãȯÀÏ
2016. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1160-1161
Transition Characteristics of Dual Bell Nozzles with Extension Length
Jeonghoon Kim, Junsub Choi, Hwanil Huh
2016. 06.
Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-165
Effect of Inflection Angle on Transition Characteristics of Dual Bell Nozzles
Jeonghoon Kim, Junsub Choi, Hwanil Huh
2016. 06.
Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-164
Analytical Study on Two-axis Pintle Thrusters with Coupling Drive Mechanism
Jaecheong Lee, Hwanil Huh
2016. 06.
Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-163
Fundamental Experiment of a Plasma Generator for Drag Reduction Applications
Seungwon Kang, Jongin Choi, Jaecheong Lee, Hwanil Huh
2016. 06.
Conference Proceedings Europe-Korea Conference on Science and Technology 2016, EKC2016-085
ÃÊÀ½¼ÓÀ¸·Î ºñÇàÇÏ´Â ºñÇàüÀÇ Ç׷°¨¼Ò¸¦ À§ÇÑ ¿ªºÐ»ç Á¦Æ®ÀÇ ¼öÄ¡Çؼ®Àû ¿¬±¸
A numerical investigation of counter-flow jet for drag reduction at high-speed flows
À± Èñ, ÀÌÇüÁø, ÇãȯÀÏ, Á¤Àμ®
2016. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.1968~1969
Ç׷°¨¼Ò¸¦ À§ÇÑ ÇöóÁ ¹ß»ýÀåÄ¡ ¼º´É½ÃÇè
The Performance Test of Plasma Generator for Drag Reduction
°½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ
2016. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.993~994
µà¾ó º§ ³ëÁñ Àü»ê¼öÄ¡Çؼ®À» À§ÇÑ ³·ù ¸ðµ¨ Æò°¡
Evaluating Turbulence Models for Numerical Analysis of Dual Bell Nozzles
±èÁ¤ÈÆ, ÇãȯÀÏ
2016. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.98~101
°íµµº¸Á¤¿ë E-D ³ëÁñÀÇ À¯µ¿Çؼ®À» À§ÇÑ ³·ù¸ðµ¨ Æò°¡
Evaluation of Turbulence Models for the CFD of Altitude-Compensating E-D Nozzles
ÃÖÁؼ·, ÇãȯÀÏ
2016. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.4~5
º§/µà¾ó º§ ³ëÁñ ÇÉƲ Ã߷±âÀÇ ¼º´É ºñ±³ ¿¬±¸
Comparison Study of Bell and Dual-Bell Nozzle Pintle Thruster Performance
³ë¼ºÇö, ±èÁ¤ÈÆ, ÇãȯÀÏ
2016. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.251-252
ºñÇàü Ç׷°¨¼Ò¸¦ À§ÇÑ ÇöóÁ ¹ß»ýÀåÄ¡ ±âÃÊ ½ÃÇè ¿¬±¸
Study on Fundamental Test of Plasma Generator for Drag Reduction of a Vehicle
°½Â¿ø, ÃÖÁ¾ÀÎ, ÀÌÀçû, ÇãȯÀÏ
2016. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.249-250
Çѱ¹Çü¹ß»çü¸¦ ±â¹ÝÀ¸·Î ¼³°èÇÑ µà¾ó º§ ³ëÁñÀÇ ÃµÀÌ Æ¯¼º
Transition Characteristics of Dual Bell Nozzle Designed based on KSLV-II
±èÁ¤ÈÆ, ÃÖÁؼ·, ÇãȯÀÏ
2016. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.243-244
Analytical Study of Drive Mechanism for Multi-axis Pintle Thrusters
Jaecheong Lee, Hwanil Huh, Hosung Lee
2016. 03.
Proceedings of the Asian Joint Conference on Propulsion and Power 2016, AJCPP2016-090
µà¾ó º§ ³ëÁñÀÇ ¹ß»çü Àû¿ë¿¡ µû¸¥ ¼º´É °³¼± È¿°ú »ç·Ê ¼Ò°³
Review on Case Studies of Performance Gain for a Launch Vehicle with a Dual Bell Nozzle
±èÁ¤ÈÆ, ÃÖÁؼ·, ÇãȯÀÏ
2015. 12.
Á¦15ȸ ¿ìÁֹ߻çü±â¼ú ½ÉÆ÷Áö¿ò pp.B-54~B-56
¿¬µ¿ ¸ÞÄ¿´ÏÁòÀ» Àû¿ëÇÑ Ãà¼ÒÇü 2Ãà ÇÉƲ Ã߷±⠽ýºÅÛ °³³ä¼³°è
Conceptual Design of Drive Mechanism for Two-Axis Pintle Thrusters
ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.831-832
ÃÊ°í¼Ó À¯µ¿¿¡¼ ¿ªºÐ»ç Á¦Æ®ÀÇ ¿Âµµ°¡ Ç×·Â °¨¼Ò¿¡ ¹ÌÄ¡´Â È¿°ú ¿¬±¸
Study of counterflow jet temperature effect on drag reduction at hyper velocity flow
ÀÌ»óÀ±, À±Èñ, Á¤Àμ®, ÇãȯÀÏ
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.822~824
MATLABÀ» È°¿ëÇÑ °íµµº¸Á¤¿ë ED ³ëÁñÀÇ ÀÏÂ÷¿ø Çؼ® ¿¬±¸
One-Dimensional Analysis for an Altitude Compensating ED Nozzle Using MATLAB
ÃÖÁؼ·, ÇãȯÀÏ
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.764~767
Çѱ¹Çü¹ß»çü È¿°À¯µµ·Î ³Ã°¢½Ã½ºÅÛ ¼³°è
Design of Gas Deflector Cooling System for KSLV-II
¿ÀÈ¿µ, °¼±ÀÏ, ÇãȯÀÏ
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.499~501
ÃÊ°í¼Ó ºñÇàü Ç׷°¨¼Ò¸¦ À§ÇÑ ÇöóÁ ºÐ»çÀåÄ¡ ¼Ò°³
Introduction to Plasma Actuation System for Drag Reduction of a High-speed Vehicle
°½Â¿ø, ±èÁöÈ«, ÀÌÀçû, ÇãȯÀÏ
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.348~350
µà¾ó º§ ³ëÁñÀ» Àû¿ëÇÏ´Â ¹ß»çüÀÇ ¼º´É À̵æ
Performance Gain of Launch Vehicles with a Dual Bell Nozzle
±èÁ¤ÈÆ, ÇãȯÀÏ
2015. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.62~64
Study of Core Technologies of a Pintle Engine for Vertical Take-off and Landing
Launch Vehicle/Lunar Module Applications
Hwanil Huh
2015. 06.
2015 CIS-Korea Conference on Science and Technology Proceedings pp.177-178
Á¤Áö±ËµµÀ§¼º Ã߷±⠰³¹ßµ¿Çâ
Development Trend of Thrusters for Geostationary Satellites
Â÷½Â¿ø, ³ëżº, ÇãȯÀÏ, ÇÑÁ¶¿µ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.527-532
°í°íµµ ȯ°æ Ã߷±â Áö»ó ½ÃÇè ¼³ºñ ÇöȲ
A Trend of Ground Test Facilities for High-Altitude Thruster
±è¿ëÂù, ³ëżº, ÇãȯÀÏ, ÇÑÁ¶¿µ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.523-526
ÇöóÁ Á¦Æ®¸¦ ÀÌ¿ëÇÑ Ç×·Â °¨¼Ò ÀåÄ¡ÀÇ ¼öÄ¡Çؼ® ¿¬±¸ »ç·Ê
Research Cases of Numerical Analysis on Drag Reduction Device using Plasma Jet
ÀÌ»óÀ±, À±Èñ, Á¤Àμ®, ÇãȯÀÏ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.710-712
ÃÊ°í¼Ó À¯µ¿¿¡¼ Á¦Æ®ºÐ»ç¸¦ ÀÌ¿ëÇÑ Ç׷°¨¼Ò¿¡ ´ëÇÑ ¹Ì±¹ÀÇ ¿¬±¸µ¿Çâ
USA Research Trends of Drag Reduction using Counter-flow Jet in High-speed Flow
ÀÌÀçû, ±èÁöÈ«, °½Â¿ø, ÇãȯÀÏ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.131~134
°íµµ º¸Á¤À» À§ÇÑ E-D ³ëÁñÀÇ ±â¼ú ºÐ¼®
Technology Review of an E-D Nozzle for Altitude Compensation Purpose
ÃÖÁؼ·, ȲÈñ¼º, ÇãȯÀÏ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.80~83
µ¶ÀÏ DLRÀÇ °íµµ º¸Á¤¿ë µà¾ó º§ ³ëÁñ ¿¬±¸°³¹ß µ¿Çâ
Recent Progress in R&D of Altitude Compensation Dual Bell Nozzle in DLR of Germany
±èÁ¤ÈÆ, ÇãȯÀÏ
2015. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.46~49
ÃÊÀ½¼Ó ³ëÁñ Ãß·Â ÃøÁ¤ ½ÇÇèÀÇ °³¼±¹æ¾È ¿¬±¸
Study on Improvement for Thrust Evaluation Experiment of Supersonic Nozzle
±èÁ¤ÈÆ, ¼È«±â
2015. 05.
Á¦3ȸ Çкλý ³í¹® °æÁø´ëȸ ³í¹®Áý pp.13~18
PE-GOX ¿¬¼Ò°¡½º ¹°¼ºÄ¡¸¦ Àû¿ëÇÑ ÇÉƲ ³ëÁñ ÇÏÀ̺긮µå ·ÎÄÏÀÇ ¼öÄ¡Çؼ® ¿¬±¸
Numerical Study on Pintle Thruster Hybrid Rockets Using Combustion Gas Properties of PE-GOX
³ë¼ºÇö, ÇãȯÀÏ
2015.05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.553~557
°íµµ º¸Á¤ ¿ÜºÎÇü ÇÉƲÃ߷±âÀÇ °íµµ¿¡ µû¸¥ ¼º´É °è»ê
Performance Estimation of the Altitude Compensating External Pintle Thruster
ÃÖÁؼ·, ÇãȯÀÏ
2015. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.549~552
°íµµ º¸Á¤¿ë ³ëÁñÀÇ ±â¼ú µ¿Ç⠺м®
Technology Trends for Altitude Compensation Nozzles
ÃÖÁؼ·, ÇãȯÀÏ
2015. 05.
Á¦14ȸ ¿ìÁֹ߻çü±â¼ú ½ÉÆ÷Áö¿ò pp.156~159
Çѱ¹Çü¹ß»çü ¹ß»ç´ë½Ã½ºÅÛ È¿°À¯µµ·Î ±âº» ¼³°è
Preliminary Design of KSLV-¥± Launch Complex Flame Deflecto r
¿ÀÈ¿µ, °¼±ÀÏ, ÀÌÁ¤ÀÏ, ¾öÇü½Ä, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.201~204
ÇÇÅä ¾Ð·Â ÃøÁ¤À» ÅëÇÑ Ãß·Â ÃøÁ¤
Thrust Evaluation from Pitot Pressure Measurements
±èÁ¤ÈÆ, ¼È«±â, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.915~916
¿ÜºÎÇü ÇÉƲÃ߷±⿡¼ Bore°¡ °ø·ÂÇÏÁß¿¡ ¹ÌÄ¡´Â ¿µÇâ
Bore Effects on Aerodynamic Loads for External Type Pintle Thrusters
ÃÖÁؼ·, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.660~661
¿¬µ¿ ¸ÞÄ¿´ÏÁòÀ» Àû¿ëÇÑ ´ÙÃà ÇÉƲ Ã߷±⠽ýºÅÛÀÇ AMESim Çؼ®¿¬±¸
Analysis of Drive Mechanism for Multi-Axis Pintle Thrusters Using AMESim
ÀÌÀçû, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.681~682
ÇÉƲ ¿òÁ÷ÀÓ¿¡ µû¸¥ ÇÉƲ Ã߷±âÀÇ Ãß·ÂƯ¼º
Pintle-Driven Thrust Characteristics of a Pintle Thruster
ȲÈñ¼º, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.817~818
ÇÉƲÃ߷±⠵¿ÀûƯ¼º¿¡ °üÇÑ ÀÏÂ÷¿ø ¼º´É¿¹Ãø
One-Dimensional Performance Prediction on Dynamic Characteristics of the Pintle Thruster
³ë¼ºÇö, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.815~816
MATLABÀ» È°¿ëÇÑ ÇÉƲ ³ëÁñÀÇ 1-DÇؼ® ¿¬±¸
One-Dimensional Analysis for a Pintle Nozzle Using MATLAB
±èÁöÈ«, ÇãȯÀÏ
2014. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.679~680
Çѱ¹Çü¹ß»çü ¹ß»ç´ë½Ã½ºÅÛ È¿°À¯µµ·Î °³³ä ¼³°è
Conceptual Design of KSLV-II Launch Complex Flame Deflector
¿ÀÈ¿µ, °¼±ÀÏ, ±è´ë·¡, ÀÌÁ¤ÀÏ, ¾öÇü½Ä, ÇãȯÀÏ
2014. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.405~410
¿¬µ¿ ¸ÞÄ¿´ÏÁòÀ» Àû¿ëÇÑ ´ÙÃà ÇÉƲ Ã߷±⠰³³ä¼³°è
Conceptual Design of Drive Mechanism for Multi-Axis Pintle Thrusters
ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º
2014. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ pp.1601~1602
±¸µ¿±â ¼Óµµ¿¡ µû¸¥ ÇÉƲ Ã߷±âÀÇ µ¿Àû Ư¼º
Dynamic Characteristics of Pintle Thruster with Pintle Speed
ȲÈñ¼º, ÇãȯÀÏ
2014. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.434~436
³ëÁñ¸ñ ³»¿ÜºÎÇü ÇÉƲÃ߷±⿡¼ÀÇ ÇÉƲ ÇàÁ¤°Å¸® ¿µÇâ
Effect of Pintle Stroke on Internal/External Pintle Thrusters
ÃÖÁؼ·, ÇãȯÀÏ
2013. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.363~366
À§Ä¡Á¦¾î ±â¹ýÀ» ÀÌ¿ëÇÑ ÇÉƲ Ã߷±âÀÇ ºñÁ¤»ó»óÅ ½ÇÇè
Unsteady-State Experiment on Pintle Thruster Using Stroke Control Method
ȲÈñ¼º, ÇãȯÀÏ
2013. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.394~397
´ÙÃà ÇÉƲ Ã߷±âÀÇ ¾Ð·ÂÁ¦¾î °³³ä¼³°è
Conceptual Design of Pressure Control for Multi-Axis Pintle Thrusters
ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º
2013. 12.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.391~393
´ÙÃà ÇÉƲ Ã߷±âÀÇ Ãß·ÂÁ¦¾î °³³ä¼³°è
Conceptual Design of Thrust Control for Multi-Axis Pintle Thrusters
ÀÌÀçû, ÇãȯÀÏ, ÀÌÈ£¼º
2013. 12.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.277~280
Áú½Ä À¯µ¿ ±¸°£À» °³¼±ÇÑ ÇÉƲ Ã߷±⿡ ´ëÇÑ ¿¹ºñ ½ÇÇè °á°ú
Preliminary Experimental Results on Pintle Thruster with Improved Choked Flow Section
ȲÈñ¼º, ÇãȯÀÏ
2013. 12.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.335~338
Toward Collaboration Efforts among EU Korean-Korean Scientists and Engineers to Facilitate Korea's Space Development Agenda
Hwanil Huh
2013. 06.
2013 EU-Korea Conference on Science and Technology(EKC) Abstract book pp.-
¿Áø°ø è¹ö¿ë ¿Á¦¾î ½Ã½ºÅÛ ÀÌÁßÈ °³³ä ¼³°è
-
¼ÈñÁØ, ÇãȯÀÏ
2013. 05.
Çѱ¹Áø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.120~120
³ëÁñ¸ñ °¡º¯ Ã߷±âÀÇ ¾Ð·ÂÁ¦¾î ±â¹ý¿¡ °üÇÑ ½ÇÇè ¿¬±¸
Experimental Study of Pressure Control Methods for Modulatable Thruster Applications
±è¼º¼ö, ȲÈñ¼º, ÇãȯÀÏ
2013. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.529~532
¸óÅ×Ä«¸¦·Î ¹æ¹ýÀ» ÀÌ¿ëÇÑ Á¤Áö±Ëµµº¹ÇÕÀ§¼º ±ËµµÀüÀÌ ÃßÁøÁ¦ ¿ÀÂ÷ºÐ¼® ¿¬±¸
GEO-KOMPSAT-2 GTO Injection Propellant Budget Error Analysis using Monte-Carlo Simulation
¹ÚÀÀ½Ä, ¹ÚºÀ±Ô, ÇãȯÀÏ
2013. 05.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.323~327
õ¸®¾ÈÀ§¼º ÀÜ¿©ÃßÁøÁ¦ ¿¹Ãø ¹× »ç¿ëÇöȲ
Residul Propellant Estimation and Consumption Status of COMS
¹ÚÀÀ½Ä, ±è¹æ¿±, ÇãȯÀÏ
2012. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.697~701
Ãæ³²´ëÇб³ ¿ìÁÖÁø°øȯ°æ ½ÇÇèÀåÄ¡¿¡ ´ëÇÑ ¼Ò°³
Introduction of Vacuum Facility at the CNU for Space Environment Tests
ÇãȯÀÏ, ±è¼º¼ö
2012. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.388~391
ÇÉƲ Çü»ó¿¡ µû¸¥ ³ëÁñ À¯µ¿º¯È¿¡ ´ëÇÑ ¿¬±¸
Effect of pintle shape on nozzle flow-pattern
À̼±°æ, ÇãȯÀÏ
2012. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.313~316
³ëÁñ¸ñ ³»/¿ÜºÎÇü ÇÉƲÃ߷±âÀÇ ¼öÄ¡Çؼ®Àû ºÐ¼®
Numerical Analysis on the Inside/Outside type of Nozzle throat Pintle thruster
±èµ¿¿¬, ±è¼º¼ö, ÇãȯÀÏ
2012. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.18~21
À¯µµ ¹Ì»çÀÏÀÇ ±ËµµÃµÀÌ ¹× ÀÚ¼¼Á¦¾î ½Ã½ºÅÛ ¿¬±¸ °³¹ß µ¿Çâ
Recent progress in Research and Development of Divert and Attitude Control System(DACS) for PGM Applications
±è¼º¼ö, ÇãȯÀÏ
2012. 04.
À¯µµ¹«±â Çмú´ëȸ ³í¹®Áý pp.243~248
SNECMA °¡º¯Ã߷±âÀÇ ÇÉƲ À̵¿°Å¸®¿¡ µû¸¥ ¼º´É ºÐ¼®
Effect of Pintle Stroke on Performance of the SNECMA Modulatable Thrust Device
¿Õ½Â¿ø, ÇãȯÀÏ
2012. 11.
Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý pp.381~382
°¡½º¹ß»ý±â ¿¬·á°³Æó ¹ëºêÀÇ ÈûÆòÇü¿¡ °üÇÑ ¿¬±¸
A Strudy on Force Balancing for a Shutoff Valve of Gas Generator
ÀÌÁß¿±, ÇãȯÀÏ
2012. 11.
Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý pp.359~360
°¡º¯ ³ëÁñ¸ñ Ã߷±âÀÇ ÇÉƲ Çü»ó¿¡ µû¸¥ Á¤»ó»óÅÂÇؼ® ¿¹ºñ°á°ú
Preliminary results of Computational Study of Steady-state Pintle driven Nozzle Throat Flow
À̼±°æ, ÇãȯÀÏ
2012. 11.
Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý pp.159~160
°¡º¯ ³ëÁñ¸ñ Ã߷±âÀÇ Á¤»ó»óÅ Ãß·Â ÃøÁ¤ ºÒÈ®µµ
Uncertainty of Steady-state Thrust Measurement for a Modulatable Thruster
À̼±°æ, ÇãȯÀÏ
2012. 06.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ
Past, Present Efforts and Future Plan of the Korean Space Vehicle Program
Hwanil Huh
2012. 06.
2012 EU-Korea Conference on Science and Technology(EKC) Abstract book pp.54-55
°¡º¯ ³ëÁñ¸ñ Ã߷±âÀÇ ÇÉƲ Çü»ó¿¡ µû¸¥ Á¤»ó»óÅÂÀ¯µ¿ ½ÇÇè ¹× ¼öÄ¡Çؼ® ¿¹ºñ°á°ú
Preliminary Results of Experimental and Computational Study of Steady-state Pintle Driven Nozzle Throat Flow
À̼±°æ, ÇãȯÀÏ
2012. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.392~396
´ÙÃà ÇÉƲ Ã߷±⠱¸µ¿ ¸ÞÄ«´ÏÁòÀÇ Æ¯Ç㠺м®
Patent Review on Drive Mechanism of Multi-Axis Pintle Thrusters Devices
±è¼º¼ö, ÇãȯÀÏ
2012. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.262~267
ÇÉƲÀÇ º¯°îÁ¡ Çü»óÀÌ SNECMA ³ëÁñ¸ñ °¡º¯ Ã߷±âÀÇ ¼º´É¿¡ ¹ÌÄ¡´Â ¿µÇâ
Effect of Pintle Inflection Points on Performance of the SNECMA Modulatable Thrust Devices
¿Õ½Â¿ø, ÇãȯÀÏ
2011. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.237~240
³ëÁñ¸ñ °¡º¯ Ã߷±âÀÇ ¾Ð·ÂÁ¦¾î ±â¹ý¿¡ °üÇÑ ¿¹ºñ½ÇÇè °á°ú
Preliminary Experimental Results of Pressure Control for Modulatable Thruster Applications
ÃÖÀ缺, ÇãȯÀÏ
2011. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.18~21
³ëÁñ ¼öÃà°¢ÀÌ SNECMA ³ëÁñ¸ñ °¡º¯ Ã߷±⠼º´É¿¡ ¹ÌÄ¡´Â ¿µÇâ
Effect of Nozzle Contraction Angle on Performance of the SNECMA Modulatable Thrust Devices
¿Õ½Â¿ø, ÇãȯÀÏ
2011. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.14~17
°í°íµµ ¿ìÁÖȯ°æ¸ð»ç¿ë Åͺ¸ºÐÀÚÆßÇÁ Áø°ø¼³ºñ ±¸Ãà
Development of Turbo Molecular Pump Vacuum Facility for High Altitude Space Environment Test
ÇãȯÀÏ, ±è¹ÎÀç, ±è¼º¼ö
2011. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.827~829
³ëÁñ¸ñ °¡º¯ Ã߷±â Àû¿ë ¸ñÀûÀÇ ÇÉƲ Çü»ó¿¡ ´ëÇÑ Á¤»ó»óÅ ½ÇÇè ¿¬±¸
Steady State Experimental Study of Pintle Shape for Modulatable Thruster Applications
ÃÖÀ缺, ÇãȯÀÏ
2011. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.153~156
³ëÁñ¸ñ °¡º¯ Ã߷±⿡¼ Bore°¡ ±¸µ¿±âÀÇ °ø·ÂÇÏÁß¿¡ ¹ÌÄ¡´Â ¿µÇâ
Effect of Bore an Aerodynamic Loads in Modulatable Thrust Devices
¿Õ½Â¿ø, ÇãȯÀÏ
2011. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.189~192
Àü±â µ¿·Â Personal Air VehicleÀÇ ÃßÁø½Ã½ºÅÛ ÇöȲ ¹× Àü¸Á
The Status and outlook of Propulsion System for Electric Powered Personal Air Vehicles
À̼±°æ, ÇãȯÀÏ
2011. 05.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.183~186
µ¥µå¹êµå¸¦ ÀÌ¿ëÇÑ °¡½º¾Ð·ÂÁ¦¾î
Pressure Control of a gas using Dead Band
ÀÌÁß¿±, ÇãȯÀÏ
2010. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý
GOx/PE ÇÏÀ̺긮µå ·ÎÄÏÀÇ Æ÷Æ® Á÷°æ¿¡ µû¸¥ ¿¬¼ÒƯ¼º ¿¬±¸
Study on Combustion Characteristic of GOx/PE Hybrid Rocket According to Port Diameter
ÃÖÀ缺, ÇãȯÀÏ
2010. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.692~693
Àú±ËµµÀ§¼º ±¤ÇОÀçüÀÇ ¿Áø°ø½ÃÇè °á°ú¸¦ ÀÌ¿ëÇÑ ¿Çؼ® ¸ðµ¨ º¸Á¤
The Correlation of Thermal Analysis Model using Results of LEO Satellite Optical Payload's Thermal Vacuum Test
±è¹ÎÀç, ÇãȯÀÏ, ±è»óÈ£, Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø
2010. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 620~621
ÇÑÁö ¸âºê·¹ÀÎÀ» »ç¿ëÇÑ ´©¼¾ÆßÇÁÀÇ È¿À² ºÐ¼®
Efficiency Analysis of Knudsen Pump According to Hanji Membrane
À±µ¿ÀÍ, ÇãȯÀÏ
2010. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.618~619
SNECMA °¡º¯³ëÁñ¸ñ Ã߷±⿡ ´ëÇÑ ¼öÄ¡Àû ¿¬±¸
Numerical Analysis of a SNECMA Modulatable Thruster Device
¿Õ½Â¿ø, ÇãȯÀÏ
2010. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.616~617
KSLV-1 ¹ß»çü ¿¬¼Ò ÈÄ·ù°¡ ¹ß»ç´ë ÁÖÀ§ ¼³ºñ¿¡ ¹ÌÄ¡´Â ¿µÇâ¿¡ ´ëÇÑ ¿¬±¸
A Study for the Effects of Exaust Gases of KSLV-1 Launch Vehicle Around the Launch Pad
°¼±ÀÏ, ¶ó½ÂÈ£, ÇãȯÀÏ
2010. 10.
Á¦ 6ȸ Çѱ¹À¯Ã¼°øÇÐ Çмú´ëȸ ³í¹®Áý
¾×ü·ÎÄÏ¿£Áø¿ë ¹ëºêÀÇ ¼Ò°³
Introduction of the Valves for Liquiid rocket engine in Launch Vehicle
ÀÌÁß¿±, ÇãȯÀÏ
2010. 08
Á¦ 6ȸ Çѱ¹À¯Ã¼°øÇÐ Çмú´ëȸ
Study on The 15th Century Korean Rocket, Dae-Sin-Gi-Jeon and Thrust Control of Hybrid Rocket
ÇãȯÀÏ
2010.
International Symposium IB-21
ÇÉƲ Çü»óÀÌ °¡º¯ ³ëÁñ¸ñ ÇÉƲ Ã߷±âÀÇ ³ëÁñ À¯µ¿¿¡ ¹ÌÄ¡´Â ¿µÇâ
Effect of Pintle on Nozzle Flow Characteristics of Variable Nozzle Thrat Area Pintle Thrusters
ÀÌ¿ë¿ì, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.275~278
ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î¸¦ À§ÇÑ Ãß·Â ¼·µ¿ °¨¼è¿¡ °üÇÑ ¿¬±¸
Suppression of Thrust Oscillation for Hybrid Rocket Thrust control Applications
°¿Ï±Ô, ÃÖÀ缺, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.197~201
DACS ±â¼úÀ» Àû¿ëÇÑ ¹Ì»çÀÏ ¹æ¾î ½Ã½ºÅÛÀÇ °³¹ßÇöȲ ¹× Àü¸Á
Development Status and Outlook of the Defence System with DACS
ÀÌ¿ë¿ì, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.402~405
GOx/PC, GOx/PE ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ½ÇÇè
Thrust Control of GOx/PC, GOx/PE Hybrid Rocket
°¿Ï±Ô, ÃÖÀ缺, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.325~328
PAV¿ë Àü±âÃßÁø ½Ã½ºÅÛÀÇ ÇöȲ ¹× Àü¸Á
The Status and Outlook of Electric Propulsion System for PAV(Personal Air Vehicle)
À±µ¿ÀÍ, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.398~401
À§¼º±¤ÇОÀçüÀÇ ¿Áø°ø½ÃÇè Áֱ⿡ µû¸¥ ¿Çؼ®
Thermal Analysis of satellite's Optical Payload through Thermal Vacuum Test Cycle
ÀÌÁ¾·ü, °¿Ï±Ô, Àå¼ö¿µ, ÀÌ´ö±Ô, ÀÌ¿õ½Ä, À̽ÂÈÆ, ÃÖÇØÁø, ÇãȯÀÏ
2010. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.502~505
STUDY ON THE 15TH CENTURY KOREAN ROCKET, DAE-SIN-GI-JEON
ÇãȯÀÏ, ÀÌ¿ë¿ì, 俬¼®
2009. 10.
60th International Astrinautical Congress
Experimental Study On the 15th Century Korean Rocket, Dae-Sin-GiN
ÇãȯÀÏ
2009. 09.
UK-Kerea Conference 2009s
°í°íµµ ¿ìÁÖȯ°æ¸ð»ç¿ë ¿Áø°øè¹ö ±¸ÃàÀ» À§ÇÑ Áø°øè¹ö °³¼±¹æ¾È
Improvement plan of Vacuum Chamber for High Altitude Space Thermal Environment Test
±èÇýȯ, ½Å°Ã¢, À±µ¿ÀÍ, ÇãȯÀÏ(Ãæ³²´ëÇб³), À¯ÀçÈ£(Çѱ¹Ç×°ø¿ìÁÖ»ê¾÷)
2009. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.627~630
´ë½Å±âÀü º¹¿ø ¿¬±¸ : ¾àÅëÀÇ ¿¬¼Ò½ÇÇèÀ» Áß½ÉÀ¸·Î
Restoration Project of the Dae-Sin-Gi-Jeon(the 15th Korean Missile)
ÀÌ¿ë¿ì, ±è¹ÎÀç, ¿Õ½Â¿ø, ±èÀçÈ£, ÇãȯÀÏ(Ãæ³²´ëÇб³), 俬¼®(Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø)
2009. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.701~704
Àú±Ëµµ À§¼ºÀÇ ¿Áø°ø½ÃÇèÀ» À§ÇÑ ¿¹ºñ ¿Çؼ®
Preliminary Thermal Analysis for LEO Satellite's Thermal Vacuum Test
ÀÌÁ¾·ü, ÇãȯÀÏ(Ãæ³²´ëÇб³), ±è»óÈ£(Çѱ¹Ç×°ø¿ìÁÖ»ê¾÷), Àå¼ö¿µ, ÀÌ´ö±Ô, ÀÌÀÀ½Ä, À̽ÂÈÆ, ÃÖÇØÁø(Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø)
2009. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.742~745
°í°íµµ ¿ìÁÖȯ°æ ¸ð»ç¿ë Áø°øè¹ö¸¦ ÀÌ¿ëÇÑ ´©¼¾ÆßÇÁÀÇ ¿¬±¸¿Í ¿Áø°øè¹ö·ÎÀÇ °³¼± ¹æÇâ
Study of Knudsen Pump using Vacuum Chamber and It's Upgrade to Thermal Vacuum Chamber
±èÇýȯ, ÇãȯÀÏ
2009. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.361~364
¿¬·áÀüÁö °³Áú±â·Î È°¿ëÀ» À§ÇÑ Swiss-roll ¿¬¼Ò±âÀÇ Å©±â¿Í ¿¬·áÀÇ Á¾·ù¿¡ µû¸¥ Ư¼º¿¬±¸
Study of Scale and Fuel type on Heat-recirculation Combustor Performance for Fuel Cell Reformer Application
±è¿¬È£, ¿ÀÈ¿µ, ÇãȯÀÏ, Paul D. Ronney
2009. 05.
´ëÇѱâ°èÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.467~468
¿¬·áÀüÁö °³Áú±â·Î È°¿ëÀ» À§ÇÑ ½ºÀ§½º·Ñ ¿¬¼Ò±âÀÇ ¿ÀüµµÀ²°ú ä³ÎÆø °¨¼Ò¿¡ °üÇÑ Æ¯¼º¿¬±¸
Effect of Thermal Conductivity and Channel width on Swiss-roll combustor performance for Fuel Cell Reformer Applications
½Å°Ã¢, ÇãȯÀÏ, Paul D. Ronney
2009. 05.
´ëÇѱâ°èÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.469~470
°¡½º¹ß»ý±â »êÈÁ¦ °³Æó¹ëºêÀÇ ³»ºÎ À¯µ¿Æ¯¼º ¹× ±¸Á¶ ¾ÈÁ¤¼º¿¡ ´ëÇÑ ¿¬±¸
Study on Flow Characteristics and Structural Analysis of Gas Generator Oxidizer Valve
ÀÌÁ¾·ü, ÇãȯÀÏ(Ãæ³²´ëÇб³), ¾È¾ç¿ì(½Ã¹Ä¶óÀÎ)
2009. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.537~540
¿Àû¹ß»êÈ¿°ú¸¦ È°¿ëÇÑ ½Å°³³ä ¼ÒÇü ÃßÁø½Ã½ºÅÛ
New Micro-propulsion System concept Using Thermal Transpiration Effect
¹ÚÀÀ½Ä(Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø), ÇãȯÀÏ(Ãæ³²´ëÇб³ )
2009. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.621~624
PAV¿ë ÃßÁø½Ã½ºÅÛ ±â¼ú ºÐ¼®
Technology Review of Propulsion System for PAV(Personal Air Vehicle)
À±µ¿ÀÍ, ÇãȯÀÏ(Ãæ³²´ëÇб³), ¾ç¼ö¼®(Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø)
2009. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 633~636
À§¼º ±¤ÇОÀçüÀÇ ¿Áø°ø ½ÃÇè ¿ÂµµÁ¶°Ç ºÐ¼®
Analysis of Thermal Vacuum Test Conditions for Satellite's Optical Payload
ÀÌÁ¾·ü, ÇãȯÀÏ(Ãæ³²´ëÇб³), Àå¼ö¿µ, ÀÌ´ö±Ô, À̽ÂÈÆ, ÃÖÇØÁø(Çѱ¹Ç×°ø¿ìÁÖ¿¬±¸¿ø)
2009. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1029~1032
PAV¿ë ¹Ì·¡Çü ÃßÁø±â°üÀÇ ÇöȲ ¹× Àü¸Á
Propulsion System for PAV Development : Now and Tomorrow
À±µ¿ÀÍ, ÇãȯÀÏ
2009. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.305~308
UAV ÃßÁø±â°üÀÇ ÇöȲ ¹× Â÷¼¼´ë UAV ÃßÁø±â°üÀÇ °³¹ß Àü¸Á
The Present State of UAV Propulsion and Forecast of Next Generation UAV Propulsion
À̵¿ÈÆ, Æر⼮, ±èÀ¯ÀÏ, ¹ÚºÎ¹Î, ÃÖ¼º¸¸, ÇãȯÀÏ
2009. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.557~560
15¼¼±â Á¶¼±½Ã´ë ·ÎÄÏÀÎ ´ë½Å±âÀü º¹¿ø : ºñÇà½ÇÇè °á°ú
The 15th Century Korean Rocket Dae-Sin-Gi-Jeon : Flight Test Result
ÀÌ¿ë¿ì, ÇãȯÀÏ
2009. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.325~328
Çѱ¹ÃßÁø°øÇÐȸ - ¿ì¼ö¹ßÇ¥³í¹®»ó ¼ö»ó! (2010³â 5¿ù 27ÀÏ)
GOx/PC ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ȯ°æ¿¡¼ ÈÄÅð°Å¸® ¿¹Ãø
Estimation of Propellant Consumption during Thrust Control of GOx/PC Hybrid Rocket
°¿Ï±Ô, ÇãȯÀÏ
2009. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.526~529
¿¬·áÀüÁö¿¡ÀÇ Àû¿ëÀ» À§ÇÑ ¼ÒÇü Çöó½ºÆ½ ¿¬¼Ò±âÀÇ Å©±â¿¡ µû¸¥ Ư¼º ¿¬±¸
Scale effect on the performance of small scale plastic combustors for fuel cell applications
½Å°Ã¢, ÇãȯÀÏ, Paul D. Ronney
2008. 12.
Á¦ 37ȸ KOSCO SYMPOSIUM ³í¹®Áý pp.206~209
´ë½Å±âÀü º¹¿ø : ¾àÅë¿¡ ´ëÇÑ ±âÃÊ¿¬±¸
To Restore the Dae-Sin-Gi-Jeon : Foundational Study of Propellant Case(Yak-tong)
ÀÌ¿ë¿ì, ±è¹ÎÀç, ¿Õ½Â¿ø, ±èÀçÈ£, ÇãȯÀÏ
2008. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.899~902
ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ¼º´É
Thrust Control Performance for Hybrid Rocket
ÀÌ¿ë¿ì, À±µ¿ÀÍ, °¿Ï±Ô, ÀÌÁ¾·ü, ±èÇýȯ, ÇãȯÀÏ
2008. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.903~906
´©¼¾ÆßÇÁÀÇ ¹è¾Ð¿¡ µû¸¥ È¿À²ºÐ¼®
Efficiency Analysis of Knudsen pump According to Back Pressure under Vacuum Condition
±èÇýȯ, ÇãȯÀÏ
2008. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.907~910
Çѱ¹ÃßÁø°øÇÐȸ - ÃÖ¿ì¼ö³í¹®»ó ¼ö»ó! (2009³â 5¿ù 14ÀÏ)
ÃʼÒÇü ÃßÁøÀåÄ¡¿¡ Àû¿ëÀ» À§ÇÑ ´©¼¾ÆßÇÁÀÇ ¸âºê·¹ÀÎ Á¾·ù¿¡ µû¸¥ ÁúÀ¯·® Ư¼º
Mass flow rate of Knudsen pump According to Membrane Type for Micro Propulsion Applications
±èÇýȯ, ÇãȯÀÏ
2008. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.36~40
Micro-Nozzle Performance and Thermal Transpiration Based Self Pumping in Vacuum Conditions
Hwanil Huh
2008. 06.
AIAA 38th Fluid Dynamics Conference and Exhibit
Æú¸®À̵̹å ÀçÁúÀÇ ¼ÒÇü Çöó½ºÆ½ ¿¬¼Ò±âÀÇ Å©±â¿¡ µû¸¥ Ư¼º ¿¬±¸
Study of scale on small polyimide combustor performance
½Å°Ã¢, ÇãȯÀÏ, Paul D. Ronney
2008. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.45~48
Á¶¼±½Ã´ë ·ÎÄÏÀÎ ´ë½Å±âÀü º¹¿ø : ¾àÅë¿¡ ´ëÇÑ ±âÃÊ¿¬±¸
The First Korean Rocket Dae-Sin-Gi-Jeon : Study of Propellant Case(Yak-Tong)
ÀÌ¿ë¿ì, ±è¹ÎÀç, ¿Õ½Â¿ø, ±èÀçÈ£, ÇãȯÀÏ
2008.11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.211~214
ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·ÂÁ¦¾î ±â¹ý¿¡ ´ëÇÑ ±âÃÊ¿¬±¸
Preliminary Study of Thrust control for Hybrid Rockets
À±µ¿ÀÍ, °¿Ï±Ô, ÀÌ¿ë¿ì, ÀÌÁ¾·ü, ÇãȯÀÏ
2008. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.257~260
°¡½ºÅÍºó ¿£Áø ȸÀü¿¬·á³ëÁñÀÇ ¿À¸®Çǽº º¯È°¡ ȸÀüºÐ¹«Æ¯¼º¿¡ ¹ÌÄ¡´Â ¿µÇâ
Effect of Orifice Variation of Rotary Atomizer on Rotating Fuel Spary Characteristics for Gas Turbine Engine
À̵¿ÈÆ, ÃÖÇö°æ, ÃÖ¼º¸¸, À¯°æ¿ø, ÇãȯÀÏ
2008. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.805~808
Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration
Based Self Pumping in Vacuum Conditions
Sungchul Jung, Hwanil Huh
2008. 03.
Asian Joint Conference on Propulsion and Power
¿ìÁÖȯ°æ¿¡¼ÀÇ ¸¶ÀÌÅ©·Î ÃßÁø
Micro Propulsion under High Altitude Space Environments
Á¤¼ºÃ¶, ÇãȯÀÏ
2008. 03.
Á¦ 5ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý
ÇÏÀ̺긮µå ·ÎÄÏÀÇ Ãß·Â Á¦¾î ¹æ¹ý¿¡ ´ëÇÑ ¿¹ºñ ½ÇÇè °á°ú
Preliminary Experimental Results of Thrust control for Hybrid rocket
ÀÌ¿ë¿ì, À̹ÎÀç, ÀÌÁ¾·ü, Á¤¼ºÃ¶, ±èÇýȯ, ÇãȯÀÏ
2007. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.237~240
Áø°øȯ°æ¿¡¼ ¿Àû¹ß»ê¿ø¸®ÀÇ ¹è¾Ð¿¡ µû¸¥ È¿À²ºÐ¼®
Efficiency Analysis of Thermal Transpiration According to Back Pressure under Vacuum Condition
Á¤¼ºÃ¶, ÇãȯÀÏ
2007. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý 76~79
Ãæ³²´ëÇб³ °í°íµµ ¿ìÁÖȯ°æ¸ð»ç Áø°ø¼³ºñÀÇ ±¸Ãà ¹× ¼º´É½ÇÇè
Development and Performance Ttest of Vacuum Facility at the CNU for High Altitude Space Environment Test
Á¤¼ºÃ¶, ±è¿¬È£, ½Å°Ã¢, ÇãȯÀÏ
2007. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.45~48
°¡½ÃÈ¿Í PDA ÃøÁ¤À» ÅëÇÑ Åͺ¸Á¦Æ®¿£Áø ȸÀü¿¬·á³ëÁñÀÇ ¹Ì¸³È Ư¼º ¿¬±¸
A Study on Atomization Characteristics of Rotating Fuel Nozzle using Spray Visualization and PDA Measurement
for Small Turbo Jet Engine
À̵¿ÈÆ, ÃÖ¼º¸¸, ÃÖÇö°æ, ÇãȯÀÏ
2007. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1424~1427
°í°íµµ ¿ìÁÖȯ°æ¸ð»ç¿ë Áø°ø½ÇÇèÀåÄ¡ ±¸Ãà
Vacuum Facility for High altitude Space Environment Test
½Å°Ã¢, Á¤¼ºÃ¶, ÇãȯÀÏ
2007. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1453~1456
Å©±â¿Í ¿¬·áÀÇ Á¾·ù¿¡ µû¸¥ Swiss-roll ¿¬¼Ò±âÀÇ Æ¯¼º¿¬±¸
Study of scale and fuel type on heat-recirculation comnbustor performance
±è¿¬È£, ¿ÀÈ¿µ, ÇãȯÀÏ, Paul D. Ronney
2007. 05.
Á¦ 35ȸ Çѱ¹¿¬¼ÒÇÐȸ KOSCO SYMPOSIUM ³í¹®Áý pp.122~126
Ãæ³²´ëÇб³ °í°íµµ ¿ìÁÖȯ°æ¸ð»ç Áø°ø½ÇÇè ÀåÄ¡
Vacuum Facility at the CNU for High Altitude Space Environment Test
½Å°Ã¢, À̹ÎÀç, Á¤¼ºÃ¶, ±è¿¬È£, ±èÇýȯ, ÇãȯÀÏ
2007. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.49~52
¿Àû¹ß»ê¿ø¸®¸¦ ÀÌ¿ëÇÑ ¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ ´ëÇÑ ¿¬±¸
Study of Micro Propulsion System Basecd on Thermal transpiration
Á¤¼ºÃ¶, ½Å°Ã¢, ±è¿¬È£, ±èÇýȯ, ÀÌ¿ë¿ì, ÇãȯÀÏ
2007. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.25~29
¸¶ÀÌÅ©·Î ³ëÁñÀÇ À¯µ¿¼Õ½Ç°ú ½Å°³³ä ÃßÁøÀåÄ¡
Flow Loss of Micro-nozzle and New Conceptual Propulsion System
Á¤¼ºÃ¶, ½Å°Ã¢, ±è¿¬È£, ÇãȯÀÏ, ¸í³ë½Å
2007. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.964~967
Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration
Based Self Pumping in Vacuum Conditions
Sungchul Jung, Hwanil Huh
2007. 04.
JSASS-KSAS Joint International Symposium on Aerospace Engineering pp.208~215
Effect of Scale and fuel type on heat-recirculation combustor performance
Younho Kim, Hwanil Huh, Jeongmin Ahn, Paul D. Ronney
2007. 03.
5th US Combustion Meeting Organized by the Western States Section
of the Combustion Institute and Hosted by the University of California at San Diego
Effect of Scale and geometry on the performance of Heat-Recirculating Swiss roll comnbustors
Hwayoung Oh, Younho Kim, Hwanil Huh, Paul D. Ronney
2007. 05.
6th Asia-Pacific conference on Comnbustion pp.538~541
¿ìÁÖȯ°æ¸ð»ç Áø°ø½ÇÇè ½Ã¼³¿¡¼ÀÇ ¹Ì¼ÒÃß·Â ÃøÁ¤¹æ¹ý
Method of Micro-thrust Measurement in Vacuum Chamber for Space Applications
Á¤¼ºÃ¶, ½Å°Ã¢, À̹ÎÀç, ±èÇýȯ, ÇãȯÀÏ
2006. 11.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.67~70
Å©±â¿¡ µû¸¥ ½ºÀ§½º·Ñ ÇüÅÂÀÇ ¿¬¼Ò±âÀÇ ¼º´É º¯È
Effects of Size on the Performance of Heat-Recirculating Swiss-roll combustors
¿ÀÈ¿µ, ±è¿¬È£, ÇãȯÀÏ, Paul D. Ronney
2006. 10.
Á¦ 33ȸ KOSCO SYMPORSIUM ³í¹®Áý pp.46~49
¸¶ÀÌÅ©·Î °íü ·ÎÄÏÀÇ ¼º´É Çâ»óÀ» À§ÇÑ ¿¬±¸
A Study for Enhanced Performance of Micro Solid-Rocketon
Á¤¼ºÃ¶, À̹ÎÀç, ±è¿¬È£, ÇãȯÀÏ
2006. 03.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.393~397
ÀúÁø°ø»óÅ¿¡¼ ³ëÁñ ÆØâºñ¿Í ºñ¿ºñ¿¡ µû¸¥ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ Æ¯¼º ¿¬±¸
Characteristic Study of Micro-Nozzles according to the Ratios of Nozzle Expansion and Specific heats in low vacuum condition
±è¿¬È£, Á¤¼ºÃ¶, ÇãȯÀÏ
2006. 08.
Á¦ 4ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý pp.249~252
¸¶ÀÌÅ©·Î ³ëÁñ À¯µ¿Àå¿¡ °üÇÑ CFD ¿¹Ãø °ËÁõ
A Validation Study on the CFD Prediction of Flow Fields in a Micronozzle
¼ÁöÇÑ, ¹Ú¹ÎÁÖ, ¸í³ë½Å, ÇãȯÀÏ
2006. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý
Effect of Geometry and Scale on the Performance of Swiss-roll combustor for Micro Power Generation
Hwayoung Oh, Hwanil Huh, Jeongmin Ahn, Paul D. Ronney
2006. 08.
The Combustion Institute 31st International Symposium, Germany
Effect of Scale on the performance of Heat-Recirculating Reactors
Hwayoung Oh, Hwanil Huh, Jeongmin Ahn, Paul D. Ronney
2006. 06.
4th International Energy Conversion Engineering Conference and Exhibit(IECEC)
Calculation of Combustion Stability Limits Using Linear Stability Analysis in Liquid Rocket Engines
Chaehoon Sohn, Isun Park, Yoonwan Moon, Hwanil Huh
2005. 10.
ÀϺ»Ç×°ø¿ìÁÖÇÐȸ ¹ßÇ¥³í¹®Áý
Research Activities on Aerospace Propulsion at Chungnam National University
Hwanil Huh
2005.
Korean-American Scientists and Engineers Association
Liquid Film Cooling in Liquid Rocket Combustor
Haeseung Jeong, Youngsung Ko, Hwanil Huh, Yoo Kim
2005. 10.
ÀϺ»Ç×°ø¿ìÁÖÇÐȸ ¹ßÇ¥³í¹®Áý
³ëÁñ ÆØâºñ¿Í ºñ¿ºñ¿¡ µû¸¥ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ Æ¯¼º¿¬±¸
Characteristic Study of Micro Nozzle According to the Ratio of Nozzle Expansion and Specific heats
¿ÀÈ¿µ, ÇãȯÀÏ, ¹®¼ºÈ¯
2005. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.381~385
°íüÃßÁø ¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ ´ëÇÑ ±âÃʽÇÇè
Fundamental Experiment for Solic Propellant Micro propulsion Device
±è¿¬È£, Á¤¼ºÃ¶, ¿ÀÈ¿µ, ÇãȯÀÏ
2005. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.39~43
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 Engine
¼ÕÀçÈÆ, ¹ÚÀ̼±, ¹®À±¿Ï, ±èÈ«Áý, ¿ÀÈ¿µ, ÇãȯÀÏ
2005. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.189~193
¸¶ÀÌÅ©·Î ³ëÁñÀÇ Ãß·ÂƯ¼º
Thrust Characteristics of Micro Nozzle
¿ÀÈ¿µ, ÇãȯÀÏ, ¹®¼ºÈ¯
2005. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.512~516
¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ ´ëÇÑ ±âÃʽÇÇè
Preliminary Experiment for Micro Propulsion Device
ÇãȯÀÏ, ¹®¼ºÈ¯, ¿ÀÈ¿µ
2005. 04.
Çѱ¹ MEMS Çмú´ëȸ ³í¹®Áý pp.122~126
ÃʼÒÇü Ã߷±â·Î¼ÀÇ Micropropulsion SystemÀÇ ÀÌ¿ë¿¡ °üÇÑ Å½»ö ¿¬±¸
-
°¼±ÀÏ, ÇãȯÀÏ, ¿ÀÈ¿µ, ¹®¼ºÈ¯
2005. 04.
Çѱ¹¿ìÁÖ°úÇÐȸ ¹ßÇ¥³í¹®Áý
Áø°ø»óÅ¿¡¼ÀÇ ¸¶ÀÌÅ©·Î ³ëÁñÀÇ Ãß·ÂƯ¼º
Thrust Characteristics of Micro Nozzle in Vacuum Condition
¿ÀÈ¿µ, ±è¿¬È£, ÇãȯÀÏ, ¸í³ë½Å
2005. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.401~404
A Study of Regenerative Cooling in a Liquid rocket Combustor
Haeseung Jeong, Heeho Park, Hwanil Huh
2004.11.
KSAS-JSASS Joint Symposium on Aerospace Engineering pp.601~604
Preliminary Experiments on Micro Cold Gas Thrust
Seonghwan Moon, Hwatyoung Oh, Hwanil Huh
2004. 11.
KSAS-JSASS Joint Symposium on Aerospace Engineering pp.274~278
½ºÅܸðÅ͸¦ ÀÌ¿ëÇÑ ÇÏÀ̺긮µå ·ÎÄÏÀÇ »êÈÁ¦ À¯·® Á¶Àý
Oxidizer Flow Control of Hybrid-Rocket using Stepping Motor
¿ÀÈ¿µ, ¹®¼ºÈ¯, ÇãȯÀÏ
2004. 08.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.601~604
¸¶ÀÌÅ©·Î ³ëÁñÀÇ ¼º´É Æò°¡
Performance Test of Micro-Nozzle
¹®¼ºÈ¯, ¿ÀÈ¿µ, ÇãȯÀÏ
2004. 08.
Á¦ 3ȸ Çѱ¹À¯Ã¼°øÇÐ Çмú´ëȸ ³í¹® ÃÊ·ÏÁý pp.103
HTPB/GO2 ÇÏÀ̺긮µå ·ÎÄÏÀÇ »êÈÁ¦ À¯·®Á¦¾î
Flow Rate Control of Gaseous Oxygen for a HTPB/GO2 Hybrid Rocket
¿ÀÈ¿µ, ¹®¼ºÈ¯, ÇãȯÀÏ
2004. 10.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.251~254
ÇÏÀ̺긮µå ·ÎÄÏ »êÈÁ¦ À¯·®Á¦¾î ½ÇÇèÀÇ ÃøÁ¤ ºÒÈ®µµ
Measurement Uncertainly of Oxidizer Flowrate Control System for a Hybrid Rocket
¿ÀÈ¿µ, ¹®¼ºÈ¯, ÇãȯÀÏ
2004. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.937~940
Navier-Stokes CFD ¸ðµ¨À» ÀÌ¿ëÇÑ ¼ÒÇü ³ëÁñ À¯µ¿Àå Çؼ®
Analysis of Flow Fields in a Small Scale Nozzle Using a Navier-Stokes CFD Model
ÇѸí½Å, ¼ÁöÇÑ, ¸í³ë½Å, ÇãȯÀÏ
2004. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.699~702
¼±Çü ¿¬¼Ò ºÒ¾ÈÁ¤ Çؼ®À» ÅëÇÑ ¿¬¼Ò ¾ÈÁ¤ÇÑ°è °î¼± °è»ê
Calculation of Combustion Stability Limits Using Linear Stability Analysis
¼ÕÀçÈÆ, ¹ÚÀ̼±(Á¶¼±´ë), ¹®À±¿Ï(KARI), ¼º´ëÇö, ÇãȯÀÏ
2004. 04.
Á¦ 5ȸ ¿ìÁֹ߻çü±â¼ú ½ÉÆ÷Áö¿ò pp.149~155
¸¶ÀÌÅ©·Î ÃßÁøÀåÄ¡¿¡ ´ëÇÑ ±âÃÊ¿¬±¸
Fundamental research on Micro Propulsion System
¹®¼ºÈ¯, ¿ÀÈ¿µ, ÇãȯÀÏ, ÇÑűÕ
2004. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.613~616
¼ÒÇü ´ÜÀÏÃßÁø Ã߷±âÀÇ Ãß·Â ÃøÁ¤
Thrust Measurement of a Small Mono-Propellant Engine
±èÀÎÅÂ, ÇãȯÀÏ, Àå±â¿ø, ÇÑűÕ
2004. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.617~620
Preliminary Study of Micro Cold Gas Thrust
Seonghwan Moon, Hwayoung Oh, Hwanil Huh
2004. 03.
Asian Joint Conference on Propulsion and Power
°í°ø¸ð»ç ȯ°æ¿¡¼ÀÇ 1 lbf±Þ ´ÜÀϾ×üÃßÁøÁ¦ ·ÎÄÏ¿£Áø ¿¬¼Ò¼º´É½ÃÇè
Hot Firing Performances of 1 lbf-Liquid Monopropellant Rocket Engine under the Environment of High Altitude Simulated
±èÁ¤¼ö, Àå±â¿ø, ÇãȯÀÏ, ÇÑÁ¶¿µ, À̱ÕÈ£, Ȳµµ¼ø, ÀÌÀç¿ø, °ÁÖ¼º, Á¤Á¾·Ï, Á¶´ë±â, ±èÀÎÅÂ
2003. 03.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.189~192
ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·ÂÃøÁ¤¿¡ ´ëÇÑ ºÒÈ®µµ Æò°¡
Uncertainty Analysis of Thrust Measurement of a Supersonic Wind Tunnel
±èÇü¹Î, ÇãȯÀÏ
2003. 03.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.538~541
Çѱ¹±º»ç±â¼úÇÐȸ - ÃßÁø ºÐ¾ß ¿ì¼ö³í¹®»ó ¼ö»ó! (2003³â 8¿ù 26ÀÏ)
¾Ð·ÂÃøÁ¤°á°ú¸¦ ÀÌ¿ëÇÑ 2Â÷¿ø ÃÊÀ½¼Ó dzµ¿ÀÇ Ã߷°è»ê
Evaluation of Thrust from Pressure Measurement of a 2-D Supersonic Wind Tunnel
±èÇü¹Î, ÇãȯÀÏ
2003. 08.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.675~678
1N±Þ ÀÚ¼¼Á¦¾î¿ë Ã߷±âÀÇ °³¹ß ½ÃÇè
Development Test of 1N Attitude Control Thruster
ÀÌÀç¿ø, ±èÀÎÅÂ, Á¤¼¼¿ë, Àå±â¿ø, ȲÁ¾¼±, ÇãȯÀÏ
2003. 10.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.35~38
Evaluation of Stream Thrust of a Supersonic Wind Tunnel
Hwanil Huh, Hyungmin Kim
2003. 07.
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Comparison of Stream Thrust Measurement Methods of a Supersonic Wind Tunnel
Hwanil Huh, Hyungmin Kim
2003. 06.
39th AIAA Fluid Dynamics Conference and Exhibit
An Experimental Study of Thrust Measurement Method of Aerospace Engines
Hwanil Huh, Hyungmin Kim, Jungyong KIm
2002. 05.
2002 World vision in Technology Exchange, CNU
Assessment of Thrust From Pressure Measurement of Supersonic Combustor
Hwanil Huh, Jungyong Kim, Yoo Kim, James F.Driscoll
2002. 07.
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
´Ù¸ñÀû ¼ÒÇü Ãß·ÂÃøÁ¤±âÀÇ Á¦ÀÛ ¹× ±âÃÊ °ËÁõ½ÃÇè
Development and Preliminary Performance test of Multi-purpose small scale Thrust Measurement System
±èÇü¹Î, ±èÁ¤¿ë, ÇãȯÀÏ
2002. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.73~76
°¢ ±¹ ´ëÇп¡¼ÀÇ ÇÏÀ̺긮µå ·ÎÄÏ ¿¬±¸ °³¹ß ÇöȲ
University Activities in R>D of Hybrid Rocket
±Ç¹ÎÂù, ÇãȯÀÏ
2002. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.455~458
¼ÒÇü Ãß·ÂÃøÁ¤±â °³¹ßÀ» ÅëÇÑ Ãß·ÂÃøÁ¤¿¡ °üÇÑ ¿¬±¸
A study of Thrust Measurement by Developing Small Scale Thrust Measurement System
±èÇü¹Î, ±èÁ¤¿ë, ÇãȯÀÏ
2002. 04.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.487~490
¿£Áø¿¬¼Ò½Ç¿¡¼ ¾Æ¼¼Åæ Çü±¤À» ÀÌ¿ëÇÑ °ø¿¬ºñ ÃøÁ¤±â¹ý ¿¬±¸
An experimental investigation of air fuel ratio measurement using laser induced acetone-fluorescence for SI engines
¿À½Â¹¬, °°Ç¿ë, ¹Ú½ÂÀç, ÇãȯÀÏ
2002. 11.
2002³âµµ ±â°è°ü·Ã »êÇп¬ ¿¬ÇÕ½ÉÆ÷Áö¾ö °¿¬ ¹× ³í¹®Áý pp.31~36
¾Æ¼¼Åæ Çü±¤À» ÀÌ¿ëÇÑ °ø¿¬ºñ ÃøÁ¤±â¹ý ¿¬±¸
An Experimental Investigation of Air Fuel Ratio Measurement using Laser Induced Acetone Fluoresence
¹Ú½ÂÀç, ÇãȯÀÏ, ¿À½Â¹¬
2002. 11.
Á¦ 2ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý pp.353~356
¾Ð·ÂÃøÁ¤À» ÀÌ¿ëÇÑ ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·Â ÃøÁ¤ ¹æ¹ý¿¡ ´ëÇÑ ½ÇÇèÀû ¿¬±¸
An Experimental Study on Thrust measurement Method of Supersonic Wind Tunnel from Pressure Measurement
±èÇü¹Î, ÇãȯÀÏ
2002. 11.
Á¦ 2ȸ Çѱ¹À¯Ã¼°øÇÐ Ãß°èÇмú´ëȸ ³í¹®Áý pp.253~256
¿ìÁÖºñÇàü¿ë ÈÇÐ½Ä Ã߷±âÀÇ ÀÌ¿ë ¹× ¿¬±¸°³¹ß ÇöȲ
Space Apolication of Chemical Thruster and its State of the Art
±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö, Àå±â¿ø
2002. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1061~1065
ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·ÂÃøÁ¤¹æ¹ý¿¡ ´ëÇÑ ºñ±³ ¿¬±¸
Comparison of Thrust Measurement Methods of a Supersonic Wind Tunnel
±èÇü¹Î, ¼º´ëÇö, ÀÌÇý¿µ, ÇãȯÀÏ
2002. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.1098~1101
Review of a Supersonic Jet Flame/Shock Wave Interaction
Hwanil Huh
2001. 11.
The 3rd International Joint Symposium of Chungnam National University and Hokkaido University pp.2~5
Measured Characteristics of Flow and Combustion in Supersonic Flame/Shock Wave Interaction
Jungoung Kim, Hwanil Huh
2001. 07.
Proceedings of the Third Asia-Pacific Conference on Combustion pp.714~717
Shock Wave Effects on Supersonic Jet-like Flames
Hwanil Huh
2001.
The 5th International Joint Symposium Between Chungnam National University and Kyushu University pp.142~147
±ØÃÊÀ½¼Ó ÃßÁø±â°üÀÇ Æ¯¼º ¹× ÃÊÀ½¼Ó ¿¬¼Ò dzµ¿ ±âÃÊ ¼³°è
Characteristics of Hypersonic Airbreathing Propulsion System and Preliminary Design of Supersonic Combustion Tunnel
±èÁ¤¿ë, ÇãȯÀÏ
2001. 04.
Çѱ¹ÃßÁø°øÇÐȸ Ãá°èÇмú´ëȸ ³í¹®Áý pp.35~38
±ØÃÊÀ½¼Ó ÃßÁø±â°ü ¿¬±¸¸¦ À§ÇÑ 2Â÷¿ø ÃÊÀ½¼Ó ¿¬¼Ò dzµ¿ °³³ä ¼³°è
Conceptual Design of a 2-D Supersonic Combustion Tunnel for Hypersonic Propulsion Study
±èÁ¤¿ë, ¼Á¤¿ø, ÇãȯÀÏ
2001. 08.
Çѱ¹±º»ç°úÇбâ¼úÇÐȸ 2001³âµµ Á¾ÇÕÇмú´ëȸ ³í¹®Áý pp.552~555
ÀΰøÀ§¼º ÃßÁøÁ¦ ¼Ò¸ð·® °èÃø¹ý¿¡ °üÇÑ °íÂû
A Study on the Gauging Method for Spacecraft in Orbit
±èÀÎÅÂ, ÇãȯÀÏ, ±èÁ¤¼ö, ÃÖÇØÁø
2001. 11.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.113~116
ÇÇÅä¾Ð·ÂÀ» ÀÌ¿ëÇÑ ÃÊÀ½¼Ó dzµ¿ÀÇ Ãß·Â ÃøÁ¤¿¡ ´ëÇÑ ±âÃÊ¿¬±¸
±èÁ¤¿ë, ¼Á¤¿ø, ÇãȯÀÏ, ±è À¯
2001. 11.
Çѱ¹ÃßÁø°øÇÐȸ Á¦ 17ȸ Çмú´ëȸ ³í¹®Áý pp.75~76
Àú±Ëµµ À§¼ºÀÇ ÀÚ¼¼Á¦¾î¸ðµåº° ÃßÁøÁ¦ ¼Ò¸ðÀ²¿¡ ´ëÇÑ °íÂû
±èÀÎÅÂ, ÀÌÇý¿µ, ÇãȯÀÏ, ±èÁ¤¼ö
2001. 11.
Çѱ¹ÃßÁø°øÇÐȸ Á¦ 17ȸ Çмú´ëȸ ³í¹®Áý pp.97~98
¼ÒÇü¾×ü·ÎÄÏ¿¡¼ÀÇ »ç°í»ç·Ê °íÂû
ÇԹ̼÷, ¹ÚÈñÈ£, Á¤ÇؽÂ, ±è À¯, ÇãȯÀÏ
2001. 11.
Çѱ¹ÃßÁø°øÇÐȸ Á¦ 17ȸ Çмú´ëȸ ³í¹®Áý pp.100
PLLIF¸¦ ÀÌ¿ëÇÑ ¿¡¸ÖÁ¯ ¿¬·áÀÇ ºÐ¹«Æ¯¼º ¿¬±¸
-
¼ÈñÁØ, ÇãȯÀÏ, ¿À½Â¹¬, ÀÓ°æ½Ä, ±è±â¼±
2000. 09.
Á¦ 1ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý Á¦ 1±Ç 1È£ pp.779~782
ÃÊÀ½¼Ó ¿¬¼Ò±â³»ÀÇ ¿¬¼Ò ¹× À¯µ¿ Ư¼º
-
ÇãȯÀÏ
2000. 09.
Á¦ 1ȸ Çѱ¹À¯Ã¼°øÇÐÇмú´ëȸ ³í¹®Áý Á¦ 1±Ç 1È£ pp.791~794
±ØÃÊÀ½¼Ó ¿¬¼Ò±â³»ÀÇ À¯µ¿ ¹× ¿¬¼Ò Ư¼º¿¡ ´ëÇÑ Ãæ°ÝÆÄÀÇ ¿ªÇÒ
-
±èÁ¤¿ë, ÇãȯÀÏ
2000. 11.
Çѱ¹ÃßÁø°øÇÐȸ Á¦ 15ȸ Çмú°¿¬È¸³í¹® ÃÊ·ÏÁý pp.33
¿¡¸ÖÁ¯ ¿¬·á¸¦ ÀÌ¿ëÇÑ µðÁ©¿£ÁøÀÇ ºÐ¹« ¹× ¹è±âƯ¼º ¿¬±¸
Spray Characteristics and Exhaust Emission Tests for a Diesel Engine Using Emulsified Fuels
¿À½Â¹¬, ¼ÈñÁØ, ÇãȯÀÏ, ÀÓ°æ½Ä, ±è±â¼±
2000. 11.
Çѱ¹ÀÚµ¿Â÷°øÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.439~443
Effects of Shock Waves on a Supersonic Hydrogen-Air Jet Flame in a Model SCRamjet Combustor
Kim, J., Huh, H., Choi, J., Yoon, Y., Jeung, I
1999. 03.
The Combustion Institute (Taiwan)
ÃÊÀ½¼Ó ¼ö¼Ò-°ø±â È¿°¿¡¼ Ãæ°ÝÆÄ ¿µÇâ¿¡ ´ëÇÑ ½ÇÇèÀû ¿¬±¸
An Experimental Study of Shock Wave Effects on the Supersonic Hydrogen-Air Jet Flames
ÇãȯÀÏ
1998. 10.
Çѱ¹Ç×°ø¿ìÁÖÇÐȸ Ãß°èÇмú´ëȸ ³í¹®Áý pp.157~162
ÃÊÀ½¼Ó È®»êÈ¿° ³»ÀÇ È¥ÇÕ°ú Àç¼øȯ ¿µ¿ª¿¡ ´ëÇÑ Ãæ°ÝÆÄÀÇ ¿µÇâ
Effects of Shock Waves on the Mixing and the Recirculation zone of Supersonic Diffusion Flames
±èÁöÈ£, ÇãȯÀÏ, ÃÖÁ¤·Ä, À±¿µºó, Á¤Àμ®
1998. 01.
Á¦ 17ȸ KOSCO SYMPOSIUM ³í¹®Áý pp.123~129
½ºÅ©·¥Á¦Æ® ¸ðµ¨ ¿¬¼Ò±â ³»¿¡¼ ÃÊÀ½¼Ó ¼ö¼Ò-°ø±â È¿°ÀÇ È¥ÇÕ°ú ¿¬¼Ò¾ÈÁ¤¼º¿¡ ´ëÇÑ Ãæ°ÝÆÄÀÇ ¿µÇâ
Shock-Wave Effects on the Mixing and the Stabilization of Supersonic H2-Air Flames for SCRamjet Applications
ÇãȯÀÏ
1998. 10.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú¹ßÇ¥´ëȸ ³í¹®Áý
Effect of Shock-Wave on the Stabilization of Hydrogen Jet Flame in a Supersonic, Coflowing Air Stream
ÇãȯÀÏ
1998. 10.
Çѱ¹ÃßÁø°øÇÐȸ Ãß°èÇмú¹ßÇ¥´ëȸ ³í¹®Áý
Measured Effects of Shock Waves on Supersonic Hydrogen-Air Flames
Hwanil Huh
1996. 07.
American Institute of Aeronautics and Astronautics
Measured Properties of Supersonic Hydrogen-Air Jet Flames
Driscoll, J.F., Huh, H., Yoon, Y., Donbar, J.M.
1995. 01.
American Institute of Aeronautics and Astronautics
Measured Lengths of Supersonic Hydrogen-Air Jet Flames-Compared to Subsonic Flame Lengths and Analysis
Driscoll, J.F., Huh, H., Yoon, Y., Donbar, J.M.
1994. 12.
American Institute of Aeronautics and Astronautics 1994.12.
Measured Lengths of Supersonic Hydrogen-Air Jet Flames-Compared to
Subsonic Flame Lengths and Analysis
Yoon, Y., Donbar, J.M., Huh, H., Driscoll, J.F.
1994.
The Combustion Institute(USA)
A Supersonic Combustor with Simple Heat Addition and Area Change-Measurements and Analysis
Yoon, Y., Donbar, J.M., Huh, H., Driscoll, J.F.
1994.
The Combustion Institute(USA)
Measured Lengths of Supersonic Hydrogen-Air Jet Flames-Compared to
Subsonic Flame Lengths and Analysis
Driscoll, J.F., Huh, H., Yoon, Y., Donbar, J.M.
1994. 03.
American Institute of Aeronautics and Astronautics 1994.03.