The increase/decrease of performance and reduction of HCl by co-crystallization
along these lines is generally directly proportional to the precursors used.
That’s not what they’re doing anyway. Lithium-aluminum which is not new so they
may be taking a different approach. Lithium aluminum hydride has also been
researched extensively along with most hydrides. As with any chemical rocket
propulsion system, we really could use some new chemicals.
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
From: arocket-bounce@xxxxxxxxxxxxx <arocket-bounce@xxxxxxxxxxxxx> On Behalf Of
DH Barr
Sent: Wednesday, March 20, 2019 9:37 PM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: New Solid Propellant Company
AP --> ADN should be a performance increase and HCl reduction, no idea if the
percentages line up for, e.g., a cocrystal.
On Wed, Mar 20, 2019, 7:47 PM Troy Prideaux <troy@xxxxxxxxxxxxxxxxxxxxx
<mailto:troy@xxxxxxxxxxxxxxxxxxxxx> > wrote:
No idea. Can only speculate – CL-20 based propellant perhaps?
Troy
From: arocket-bounce@xxxxxxxxxxxxx <mailto:arocket-bounce@xxxxxxxxxxxxx>
[mailto:arocket-bounce@xxxxxxxxxxxxx ;<mailto:arocket-bounce@xxxxxxxxxxxxx> ] On
Behalf Of Charlie Garcia
Sent: Thursday, 21 March 2019 11:08 AM
To: (AR) ocket List <arocket@xxxxxxxxxxxxx <mailto:arocket@xxxxxxxxxxxxx> >
Subject: [AR] New Solid Propellant Company
These folks graced my social media feed today. I recognize some of the names on
the team, which is promising. Any speculation on their propellant? HCl exhaust
has caused me difficulty with the EHS people in my lab before. It'd be nice to
avoid it.
https://www.adranos.com/