| 분류 | 표면기술 |
|---|---|
| 기술명 | Thermal Barrier Coating for Space Launch Vehicles |
| 연구자 | Eung-sun Byon |
| 특허출원번호 | KR10-1136907 |
| 개요 | This technology is about ensuring the durability of the thermal barrier coating layer after
over 10 times of testing lasting over a total of 600 seconds, including the longest combustion of 150 seconds per test, in a thermal environment equivalent to that of the actual thrust chamber of a liquid fuel rocket engine (combustion pressure of 6-8MPa, O/F ratio of 2.4-2.5, total flow rate of 20-30 kg/s). Constituting technologies MCrAlY bond coating, VPS/APS coating ZrO2 ceramic thermal barrier coating Cylinder/nozzle interior coating, actual product coating Fabrication and mixing of spray powder with low thermal conductivity FGM-TBC coating Coating evaluation and analysis |
| 첨부파일 |  086_Thermal_Barrier_Coating_for_Space_Launch_Vehicles.jpg (633.3K) [18] DATE : 2018-02-09 17:22:28 |
![086_Thermal_Barrier_Coating_for_Space_Launch_Vehicles.jpg (633.3K) [18] DATE : 2018-02-09 17:22:28](javascript:file_download('./download.php?bo_table=tlo_03_01&wr_id=413&no=0&page=12', '086_Thermal_Barrier_Coating_for_Space_Launch_Vehicles.jpg');){kind=link}
