°í¼ÓÃßÁø ¹× ¿¬¼Ò½ÇÇè½Ç

+ ÇÑÁÙ °øÁö : ·Î±×ÀÎ ÇÏ¼Å¾ß °­ÀÇ °ü·Ã °Ô½ÃÆÇÀÇ ±ÛÀ» È®ÀÎÇÒ ¼ö ÀÖ½À´Ï´Ù.

sub menu

 

 

# Publications

 
 

 ÇмúÁö (Journal)

 

 

 Çмú´ëȸ (Conference)

 
 

 ÇÐÀ§³í¹® (Thesis)

 
 

 Book Chapter

 
 

 Æ¯Çã (Patent)

 

gadget

[ HPCL ¿¬±¸ ³»¿ë ]

ÁøÇà ¿¬±¸ °úÁ¦

Á¾·á ¿¬±¸ °úÁ¦


½ÇÇè½Ç º¸À¯ Àåºñ

 

[ 2021-2 °­ÀÇ °Ô½ÃÆÇ]

[27148-00] ºñÇàÃßÁø½ÇÇè

[24087-00] ¿¡³ÊÁö¿Í¿­Àü´Þ

*·Î±×ÀÎ ÈÄ ÀÌ¿ëÇϼ¼¿ä.

[ 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 2024

 

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 2024

 

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 Deflector

¿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.

 


   Webadmin : Hyunjin Jeong (disneyboy@naver.com)

High speed Propulsion and Combustion Laboratory : HPCL

Copyright(c) All rights reserved.