brin
Aerospace
- Mar 12, 2000
- 122
Does anyone have links or references for estimating temperature of a part exposed short term (eg: 1-2 seconds) to heat from solid rocket exhaust? I understand this will vary with location and orientation to the exhaust, but I am looking for a conservative temperature to use in comparison between different thermal barrier coatings.
Also any links to manufacturers for thermal barrier coatings would be appreciated. Note maximum coating thickness of .125 inch.
thanks
Also any links to manufacturers for thermal barrier coatings would be appreciated. Note maximum coating thickness of .125 inch.
thanks