[AR] Re: Hydroxylammoniumnitrate (HAN)

  • From: "Galejs, Robert - 1007 - MITLL" <galejs@xxxxxxxxxx>
  • To: "arocket@xxxxxxxxxxxxx" <arocket@xxxxxxxxxxxxx>
  • Date: Mon, 3 Apr 2017 15:52:18 +0000

Thanks for the ADN reference!

 

Here’s a NASA press release that says the AF-M315E does contain HAN: 
https://www.nasa.gov/mission_pages/tdm/green/overview.html

 

- Robert

 

-----Original Message-----
From: arocket-bounce@xxxxxxxxxxxxx [mailto:arocket-bounce@xxxxxxxxxxxxx] On ;
Behalf Of James Padfield
Sent: Monday, April 03, 2017 11:40 AM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: Hydroxylammoniumnitrate (HAN)

 

Looking at this link, the AF-M315E propellant does not appear to be HAN-based, 
although they are a bit vague as to what it actually is (although I may be 
wrong - as I said, it is vague!):

 

 
<http://www.rocket.com/files/aerojet/documents/Capabilities/PDFs/GPIM%20AF-M315E%20Propulsion%20System.pdf>
 
http://www.rocket.com/files/aerojet/documents/Capabilities/PDFs/GPIM%20AF-M315E%20Propulsion%20System.pdf

 

You may also be interested in LMP-103S, another hydrazine replacement 
monopropellant, this time based on ADN, developed by Eurenco and ECAPS in 
Sweden.  UN classification of 1.4S when packaged in HDPE bottles and a wooden 
box with absorbent:

 

 <http://www.dtic.mil/ndia/2009/insensitive/8Asjoberg.pdf
http://www.dtic.mil/ndia/2009/insensitive/8Asjoberg.pdf

 

 

On 3 April 2017 at 15:02, Galejs, Robert - 1007 - MITLL < 
<mailto:galejs@xxxxxxxxxx> galejs@xxxxxxxxxx> wrote:

I was under the impression that the "green" monopropellants were based 

on HAN. For example:  

 <http://www.rocket.com/green-monopropellant-propulsion
http://www.rocket.com/green-monopropellant-propulsion







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







Robert







-----Original Message-----

From:  <mailto:arocket-bounce@xxxxxxxxxxxxx> arocket-bounce@xxxxxxxxxxxxx 

[ <mailto:arocket-bounce@xxxxxxxxxxxxxmailto:arocket-bounce@xxxxxxxxxxxxx] ;
On Behalf Of Anthony Cesaroni

Sent: Saturday, April 01, 2017 3:36 PM

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