[AR] Re: Hydroxylammoniumnitrate (HAN)

  • From: "Galejs, Robert - 1007 - MITLL" <galejs@xxxxxxxxxx>
  • To: "arocket@xxxxxxxxxxxxx" <arocket@xxxxxxxxxxxxx>
  • Date: Mon, 3 Apr 2017 13:02:07 +0000

I was under the impression that the "green" monopropellants were based on
HAN. For example:  http://www.rocket.com/green-monopropellant-propulsion

 

Maybe they found the magic sauce to keep things orderly in an engine.

 

Robert

 

-----Original Message-----
From: arocket-bounce@xxxxxxxxxxxxx [mailto:arocket-bounce@xxxxxxxxxxxxx] On
Behalf Of Anthony Cesaroni
Sent: Saturday, April 01, 2017 3:36 PM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: Hydroxylammoniumnitrate (HAN)

 

I've read that citation previously. Note some of the issues. They increase
exponentially in a *steady state* liquid propellant engine or hybrid.

 

Best.  

 

Anthony J. Cesaroni

President/CEO

Cesaroni Technology/Cesaroni Aerospace

 <http://www.cesaronitech.com/> http://www.cesaronitech.com/

(941) 360-3100 x101 Sarasota

(905) 887-2370 x222 Toronto

 

-----Original Message-----

From:  <mailto:arocket-bounce@xxxxxxxxxxxxx> arocket-bounce@xxxxxxxxxxxxx [
<mailto:arocket-bounce@xxxxxxxxxxxxx> mailto:arocket-bounce@xxxxxxxxxxxxx]
On Behalf Of Uwe Klein

Sent: Saturday, April 1, 2017 10:00 AM

To:  <mailto:arocket@xxxxxxxxxxxxx> arocket@xxxxxxxxxxxxx

Subject: [AR] Re: Hydroxylammoniumnitrate (HAN)

 

Am 01.04.2017 um 15:13 schrieb John Dom:

An Abrams tank cannon liquid propellant part.

 

strangely interesting:

 <http://www.dtic.mil/get-tr-doc/pdf?AD=ADA258887>
http://www.dtic.mil/get-tr-doc/pdf?AD=ADA258887

 

Uwe

 

 

 

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