antiterror13
Brigadier
Here
You can find various other articles and report through google if you are interested.
google? of course
Here
You can find various other articles and report through google if you are interested.
Ahh, the XF5-1 engine powering the X-2 is full of ceramic engine components.
The engine temperature at the turbine entrance stage is around 1600℃ already.
In context, is an operating temperature of 900 deg C good enough for low pressure turbine blades? When the highest temperature in advanced jet engines is in excess of 1500 deg C, where does this fit in the picture?
google? of course
That was serious question @antiterror13 and I was hoping for a serious response.