I don't know the exact numbers but it could be the heat of the smoke of the rocket (for the highest temperature) and when the rocket reaches the stratosphere (for lowest temperature). 
-
-
Thanks. Twitter will use this to make your timeline better. UndoUndo
-
-
-
This Tweet is unavailable.
-
Rocket Propulsion Elements by George Sutton is great!
- Show replies
-
-
-
Basically, the hottest part of the engine , throat area. Where the mass flow rate is maximum.
Thanks. Twitter will use this to make your timeline better. UndoUndo
-
-
-
The throat
Thanks. Twitter will use this to make your timeline better. UndoUndo
-
-
-
maybe max Q for turbulence and highest friction during launch

-
and the extreme cold from the propellant?
End of conversation
New conversation -
-
-
Thanks. Twitter will use this to make your timeline better. UndoUndo
-
Loading seems to be taking a while.
Twitter may be over capacity or experiencing a momentary hiccup. Try again or visit Twitter Status for more information.
We are
