[AR] Re: Phenolic regression rate

  • From: Hagen Hübner <hagen.huebner@xxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Thu, 01 Feb 2018 21:55:38 +0100


Bill:

Some (quite restricted) "user data": A 1 mm Phenolic-Liner (Hp 2061) in a 38 mm OD casing will withstand a 1 second burn of APCP (no Al or other metals added) in a free standing BATES-grain configuration without any problems. It will be coked after a 5 second burn with the same propellant in an end-burner configutation but will still save the aluminum-casing (wall thickness 2 mm) from a burn-through (just some discoloration of the anodic coating). I can provide photos if desired.

Hagen





Troy:


Let me add that given 0.8 mm and a (conservative) 1.2 second burn, it follows that this liner was good for about 0.66 mm per >>>second, implying a need for 6.66 mm for a 10 second burn.


With enough similar data it will be possible to estimate a number, with variance, that at the low end allows for a (probably) >>>safe flight.


Bill

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