¹øÈ£ ±¸ºÐ Àå¼Ò ½ÇÇè½Ç½À½Ç¸í ´ã´ç±³¼ö ºñ°í
1 Ç×
°ø
¿ì
ÁÖ

¹×

±â
°è
°ø
ÇÐ
ºÎ
±â 103 ÃßÁø ¹× ¿¬¼Ò½ÇÇè½Ç Propulsion & Combustion Lab. ±¸ÀÚ¿¹
2 ±â 104 ¿­°øÇнÇÇè½Ç Thermal Engineering Lab. ºÎÁØÈ«
3 ±â 105 °øµ¿½ÇÇè½Ç 1 °­Å°ï
4 ±â 106 ÀÀ¿ë±âüÀ¯µ¿ ½ÇÇè½Ç Applied Gas Flow Laboratory ÀÌ¿­
5 ±â 204-A º¹ÇÕÀç·á ±¸Á¶ ½ÇÇè½Ç Composite Materials & Structures Lab. À̼ö¿ë
6 ±â 204-B °øµ¿½ÇÇè½Ç 2 ³ëÁøÈ£
7 ±â 205 ±¸Á¶½Ã½ºÅÛ°øÇÐ ½ÇÇè½Ç Structural System Engineering Lab. ¹ÚÁ¤¼±
8 ±â 206 ¿ìÁÖÇ×¹ý ½ÇÇè½Ç Spacecraft Control Lab. ±èÁ¤·¡

9

±â 207

ÃÊÁ¤¹ÐÃøÁ¤ ½ÇÇè½Ç

 

Çлç´ã´ç

ºÎÇкÎÀå

 

10 ±â 216 Àü»êÀ¯Ã¼°øÇнÇÇè½Ç Computational Flow Simulation Lab. ±è¹®»ó
11 ±â 303 Àú¼Ó°ø±â¿ªÇнÇÇè½Ç Low-Speed Aerodynamic Lab. Àå¼®ÇÊ
12 ±â 304 Ç×°ø±â¼³°è Á¦µµ½Ç Aircraft Design & Drawing Lab. ¹èÀ缺
13 ±â 402 ¸ÞīƮ·Î´Ð½º½ÇÇè½Ç Mechatronics Lab. ±èÁ¾¼±

 

14 ±â 403 ½Ã½ºÅÛ ÃÖÀû¼³°è ¿¬±¸½Ç System Design Optimization Lab. ÃÖÁÖÈ£
15 ±â 403-1 Çкΰøµ¿½ÇÇè½Ç 3

Çлç´ã´ç

ºÎÇкÎÀå

16 ±â 404 À¯Ã¼°øÇÐ ¹× ³­·ùÁ¦¾î ½ÇÇè½Ç Fluid Engineering & Turbulence Control Lab.

¹®ÈñÀå

Àüâ¼ö

17 ±â 405 ·ÎÄÏ ÃßÁø ½ÇÇè½Ç Rocket Propulsion Lab. ±èÁø°ï
18 ±â 406 Áö´É Áøµ¿Á¦¾î½Ã½ºÅÛ ¿¬±¸½Ç Intelligent Vibration Control System Lab.(IVCS) ȲÀçÇõ

19

°ú 106

À¯°ø¾ÐÁ¦¾î ½ÇÇè½Ç

Fluid Power and Motion Control Lab.

È«¿¹¼±

 

20 »ýȰ B101-1 Áö´ÉÁøµ¿Á¦¾î½Ã½ºÅÛ ¿¬±¸½Ç Intelligent Vibration Control System Lab.(IVCS) ȲÀçÇõ

21

»ýȰ B101-2

¹«ÀÎÇ×°ø½Ã½ºÅÛ ¿¬±¸½Ç

 

¼Û¿ë±Ô

 

22 ¿ì B101A ÀÀ¿ë¿ªÇÐ ½ÇÇè½Ç Applied Mechanics Lab. ¿°´ëÁØ
23 ¿ì B101B ÀÀ¿ë¿­Àü´Þ ½ÇÇè½Ç ºÎÁØÈ«
24 ¿¬ 102 ÷´Ü¹«Àα⿬±¸¼¾ÅÍ ¼Û¿ë±Ô
25 ¿¬ 103 ½ºÆäÀ̽º¸ÞÄ¿´ÏÁò¿¬±¸½Ç ±èº´±Ô
26 ¿¬ 105 À§¼ºÁ¦¾î ½ÇÇè½Ç Spacecraft Control Lab. ¿ÀÈ­¼®
27 ¿¬ 106 ¿ìÁֽýºÅÛ ½ÇÇè½Ç Space System Research Lab. À念±Ù
28 ¿¬ 107 Áö´É Áøµ¿Á¦¾î½Ã½ºÅÛ ½ÇÇè½Ç B ¹èÀ缺
29 ¿¬ 204 Ç׿ì±â °øµ¿½ÇÇè½Ç 4

±è°æ¸ñ

ÀÌÇб¸

30 ¿¬ 206 °í¼ÓÃßÁø ¹× ¿¬¼ÒÁ¦¾î ½ÇÇè½Ç ¼ºÈ«°è

31

¿¬ 306

  °íÀ忹Áö ¹× °ÇÁ¤¼º°ü¸® ½ÇÇè½Ç

 

ÃÖÁÖÈ£

 

32

¿¬ 405

  Ç׿ì±â °øµ¿½ÇÇè½Ç 5

 

ÀÌ»óö

 

33

¿¬ 407

  ¿­À¯µ¿Á¦¾î ¿¬±¸½Ç

 

°ûÀç¼ö

 

34

¿¬ 409

  BK 21»ç¾÷´Ü ½ÇÇè½Ç

 

±¸ÀÚ¿¹

 

35

¿¬ 410

  µå·Ð ºñÇà ºÐ¼®½Ç

 

°í»óÈ£

 

36

¿¬ B101

  ¿ëÁ¢°øÇÐ ½ÇÇè½Ç

 

À̽Âȯ

 

37

¿¬ B102

  ±â°è°øÀÛ ¹× ÃßÁø±â°ü ½ÇÇè½Ç

 

Çлç´ã´ç

ºÎÇкÎÀå

 

38

¿¬ B103

  dzµ¿ ½ÇÇè½Ç

 

±èÇкÀ

 

39

°­ 307

  °øµ¿½ÇÇè½Ç(D)

 

Çлç´ã´ç

ºÎÇкÎÀå

 

Ç×°ø¿ìÁÖ ¹× ±â°è°øÇкΠ¼Ò°è (39½Ç)

Áöµµ±³¼ö º° ·¦ ¼Ò°³

Áöµµ±³¼ö ·¦ ÁÖ¿ä ¿¬±¸ºÐ¾ß ¼Ò°³
ÀÚ·á
°ûÀç¼ö ¿­À¯µ¿ Á¦¾î ¿¬±¸½Ç
  • - ´Ù¾çÇÑ ÃֽнÇÇè ±â¹ýÀ» ÀÌ¿ëÇÑ À¯µ¿ ¹× ¿­Àü´Þ ½ÇÇè
  • - °¡½ºÅͺó ºí·¹À̵å À¯µ¿, ¿­Àü´Þ ¹× ³Ã°¢¿¡ ´ëÇÑ ¿¬±¸
  • - »ó¿ë Äڵ带 ÀÌ¿ëÇÑ Åͺ¸±â°è ¿­À¯µ¿ ÇØ¼®
±¸ÀÚ¿¹ Propulsion & Combustion Lab.
  • - Tested to demonstrated improved ingnition characteristic
  • - Combustor Characteristics with CFD
  • - Contour of cross-flow with KIVA & Spray structure of Cross-flow Image
  • - Triplet Injector & Spray Structure
±Ç»óÁÖ ·Îº¿½Ã½ºÅÛÁ¦¾î ¿¬±¸½Ç
  • - Control/Mechatronics
  • - Robotics
  • - Machine Vision
  • - Estimation/Filtering
±èµÎ¸¸ Ç×°ø¿ìÁÖ ±¸Á¶&Àç·á ½ÇÇè½Ç(ASML)
  • - Aircraft Structures
  • - Tire Mechanics
  • - Rubber Elasticity
±è¹®»ó Àü»êÀ¯Ã¼°øÇнÇÇè½Ç
(Computational Flow Simulation Lab)
  • - Â÷¼¼´ë ÀÚµ¿Â÷ ¿ÜÇü ¼³°è
  • - ½Â¿ëÂ÷ »çÀÌµå ¹Ì·¯ °ø·Â ¼³°è
  • - Ç×°ø±â ¾ÐÃà±â
±èº´±Ô National Space Lab -Satellite Mechanism Research Laboratory
  • - Bio MEMS(Micro Electro Mechanical System)
  • - Bio Robot
±è¼®ÀÏ »ý»êÀÚµ¿È­¿¬±¸½Ç
  • - »ý»ê ÀÚµ¿È­ °ü·Ã ¼ÒÇÁÆ®¿þ¾î ºÐ¾ß
  • - °øÀÛ±â°è / ¹ÝµµÃ¼ ÀåºñÀÇ ±¸Á¶ ¼³°è ¹× ¼º´É ÇØ¼®
±èÁ¤·¡ À§¼ºÀÀ¿ë ¿¬±¸½Ç
  • - À§¼ºÇ×¹ý ½Ã½ºÅÛ ÀÀ¿ë ¿¬±¸
  • - À§¼º ¹× ¹ß»çü °ü·Ã ¿¬±¸
±èÁ¾¼± MECHATRONICS ¿¬±¸½Ç
  • - Mobile Robot
  • - Humanoid Robot
  • - Mechatronics °ü·Ã
±èÁø°ï ÇÏÀ̺긮µå ·ÎÄÏÃßÁø¿¬±¸½Ç
(Hybrid Rocket Propulsion Laboratory)
  • - Combustion Characteristics with the Various Fuel
  • - Combustion Characteristics with the Various Oxidizer
  • - Improvement of Low Regression Rate
  • - Transient Combustion Characteristics Improvement of Combustion Efficiency
  • - Combustion Characteristics of Multi-port Grain Combustion
  • - Combustion Characteristics with the Injector type Characteristics with the Various Fuel
  • - Improvement of O/F Shift
  • - Pyrolysis Characteristics of N2O in Catalyst Bed
¹®ÈñÀå Turbulent Control & Combustion Lab. (NRL Affiliate Lab.)
  • - Multi-Port Hybrid Rocket Combustion Experiments
  • - Fundamental Study of the Regression rate mechanism
  • - End-burning Hybrid Rocket Combustion Analysis
  • - Study on the Nanofluid behavior in turbulent flow
  • - Study on the micro TPV power system
  • - Study on the micro combustor integrated with a micro reformer and a micro evaporator.
¹ÚÁ¤¼± System and Structure Optimal Design Lab.
  • - Automobile component design and analysis
  • - Non-linear analysis for fuel cell system
  • - Excavator clamp design
  • - Electric rail car design
  • - Optimal design for helicopter potor system
  • - Damage tolerant design for smart U.A.V.
  • - Structural analysis & optimization for KOMAST 2
  • - Wing analysis for T-50
¹èÀ缺 Áö´É Áøµ¿ Á¦¾î ¿¬±¸½Ç(IVCS)
  • - Áøµ¿°èÀÇ ´Éµ¿Á¦¾î
  • - À¯¿¬±¸Á¶¹°ÀÇ ÀÜ·ùÁøµ¿ Á¦¾î±â¹ý ¿¬±¸
  • - µ¿¿ªÇаèÀÇ ¸ðµ¨¸µ ¹× Á¦¾î
  • - ¸ðÇÎÇü ¹«Àα⠸ÞÄ¿´ÏÁò ¼³°è ¹× Á¦¾î
  • - Ç×°ø±â ¹× ¹ß»çüÀÇ Ç÷¯ÅÍ ¾ïÁ¦
  • - Âø·üÀåÄ¡ ¿ÏÃæ±âÀÇ µ¿Æ¯¼º ÇØ¼® ¹× ´Éµ¿Á¦¾î
  • - ¿ÍÀü·ù °¨¼è±â¸¦ ÀÌ¿ëÇÑ Áøµ¿Á¦¾î
  • - ·ÎÅÍºí·¹À̵åÀÇ µ¿Æ¯¼º
¼ºÈ«°è °í¼ÓÃßÁø ¹× ¿¬¼Ò ½ÇÇè½Ç
  • - °ø±âÈíÀÔ °í¼ÓÃßÁø
  • - ·ÎÄÏÃßÁø
  • - ´ë¿ë·® °í¼Ó¿¬»êÀ» À§ÇÑ °í¼º´É ÄÄÇ»ÆÃ
¼Û¿ë±Ô Flight Control Lab
  • - UAV(¹«ÀÎÇ×°ø±â)
  • - ³ó¾÷¿ë ¹«ÀκñÇ༱
¿ÀÈ­¼® À§¼ºÁ¦¾î½ÇÇè½Ç
  • - À§¼º ½Ã¹Ä·¹À̼Ç
  • - À§¼º ±¸µ¿±â ¼³°è ¹× °³¹ß
  • - À§¼ºÀÚ¼¼ Á¦¾î½ÃÇè
  • - ±¸µ¿±â ¼º´É½ÃÇè
À̺¸¿µ NRL for CCM & Welding Lab.
  • - ¿­ÇǷαտ­ ¹× ÀÀ·ÂºÎ½Ä±Õ¿­ Á¦ÀÛ
  • - ¿ëÁ¢ºÎ ¼Õ»óÇØ¼® ¹× ÇöÀå¿ëÁ¢°øÁ¤ ¾ÈÁ¤È­
ÀÌ»óö Ç×Àü Á¦¾î ¹× Ç×¹ý ½ÇÇè½Ç
  • - À§¼º ¹× Ç×°ø±â Á¦¾î¿Í ºñÇàÇ×¹ý¿¡ °ü·ÃµÈ °³¹ß ¹× ¿¬±¸
ÀÌ¿­ °í¼Ó°ø±â¿ªÇнÇÇè½Ç
  • - ¸¶ÀÌÅ©·Î ÃÊÀ½¼Ó Á¦Æ®À¯µ¿ Ư¼º ¹× ·¹ÀÌÀú °¡°ø ÀÀ¿ë
  • - ³ÃÀåÁø¿­´ë ¿¡¾îĿưÀÇ Æ¯¼º ¹× ¼º´ÉÇâ»ó
  • - ÃÊÀ½¼Ó °øµ¿ºÎ À¯µ¿ÀÇ Æ¯¼º ¹× Á¦¾î
  • - ¾ÆÀ½¼Ó À¯µ¿Àå Àü´ÜÀÀ·Â ¹× ¿­Àü´Þ ÃøÁ¤¹ý °³¹ß
  • - Ãæ°ÝÆÄ¿Í °æ°èÃþ °£¼·À¯µ¿ÀÇ Çǵ¿Á¦¾î
  • - ÃÊÀ½¼Ó Á¦Æ®À¯µ¿ÀÇ Thrust Vector Controls
Àå¼®ÇÊ ¸¶ÀÌÅ©·Î & ³ª³ë¿­Àü´Þ ¿¬±¸½Ç
  • - Nanofluids
  • - Cooling Technology for Electronic Packages
  • - Micro/ Nanoscale Heat Transfer and Fluid Flow Characteristics
  • - Convective Heat Transfer in Porous Media
  • - Thermal Phenomena in the Catalyst Bed for Rocket Ignition System
  • - Development of Sensors and Measurement Technology
  • - Multiport Dryer
À念±Ù ¿ìÁֽýºÅÛ ¿¬±¸½Ç(SSRL)
  • - Low-cost space missions
  • - Pico, nano, and micro-satellite technology research and development
  • - Student training (design, assembly, integration, test, LEOP and operation)
ÃÖÁÖÈ£ SDOL(System Design Optimization Lab.)
  • - °¡»ó¼º´ÉÆò°¡(CAE) ±â¼ú ÀÌ¿ë
  • - ±â°è¡¤Ç×°ø ½Ã½ºÅÛÀÇ ÃÖÀû¼³°è ¹æ¹ý ¿¬±¸
È«¿¹¼± À¯°ø¾ÐÁ¦¾î ¿¬±¸½Ç
  • - À¯°ø¾ÐÀ» ÀÌ¿ëÇÑ ·Îº¿ ±¸µ¿ÀåÄ¡
  • - ·Îº¿À» ÀÌ¿ëÇÑ Ä¸½¶Çü ³»½Ã°æÀÇ ¿ø°Ý Á¶ÀÛ ±â¼ú
  • - 4Á· º¸Çà ·Îº¿ÀÇ Çè·Î º¸Çà¿ë foot ¼³°è


¸ÇÀ§·Î