Catocene is nice in theory but a very bad player. TNO had an accident with it a
few years ago and they weren’t the first ones. It pretty much been banned by
the DoD. Same goes with ferrocene.
A good resource is Alain Davenas book “Solid Rocket Propulsion Technology”.
SNPE required reading.
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 [mailto:arocket-bounce@xxxxxxxxxxxxx] On ;
Behalf Of Bruno Berger SPL
Sent: Sunday, June 17, 2018 3:18 AM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: Fast propellant
Am 16.06.2018 um 23:39 schrieb William Claybaugh:
Does anyone have any sense of how fast AP/HTTP/Al can be made to
reliability burn at reasonable pressure (say 1000 psia)?
I’m noting that if one could get around 9-10” / sec. an end-burning
grain might makes sense with rather significant effects on propellant
fraction for sounding rockets....
Bill