[AR] Re: New Solid Propellant Company

  • From: "Anthony Cesaroni" <anthony@xxxxxxxxxxx>
  • To: <arocket@xxxxxxxxxxxxx>
  • Date: Thu, 21 Mar 2019 12:34:40 -0400

Not really. The application didn’t support slurries or suspensions. Dissolved 
was the desired end product. ADN is an odd player. Its intermediate 
decomposition step is N2O + H4N2O3. We did successfully coat HNF with 
functional NC (12% N) however. That did some very things. In particular, 
mechanical properties and compatibility.

Anthony J. Cesaroni
President/CEO
Cesaroni Technology/Cesaroni Aerospace
http://www.cesaronitech.com/
(941) 360-3100 x101 Sarasota
(905) 887-2370 x222 Toronto

-----Original Message-----
From: arocket-bounce@xxxxxxxxxxxxx <arocket-bounce@xxxxxxxxxxxxx> On Behalf Of 
Uwe Klein
Sent: Thursday, March 21, 2019 11:22 AM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: New Solid Propellant Company

Am 21.03.2019 um 15:33 schrieb Anthony Cesaroni:

I once had the bright idea that ADN and H2O2 would make a great 
mono-propellant and oxidizer. They do, immediately upon coming into 
contact unfortunately.

Any path to coating component particles before joining them into a mono 
propellant stick ?


Uwe





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