Hello Peter,Thank you for replying to my query. Unfortunately, I know nothing about the SugPro list. However, the simulation you described below sounds like just the motor we Jetex/Rapier modelers could use! At the very least, it could serve as a baseline design "point of departure" that we could start with to develop such motors. That will be quite helpful--Thank You very much!
-- Jason----- Original Message ----- From: "Peter Johansson" <rockets4kids@xxxxxxxxx>
To: <sugarshot@xxxxxxxxxxxxx> Sent: Wednesday, January 01, 2014 9:22 AM Subject: [SS2S-Main] Re: Rocket help request
On Wed, Jan 1, 2014 at 3:57 AM, James Jason Wentworth <blackshire@xxxxxxxxxx> wrote:Yesterday and today I have received numerous messages on the SS2S e-mail list. I was wondering if anyone here could offer suggestions to solve a problem:Before we get to that, Is there any news on the migration of the SugPro list to the new mail server? That list would be far more appropriate for this discussion than ss-main.something similar to this but optimized for model jet use (an end-burner producing 1/10 of a newton or so of thrust, for 10 - 20 seconds or more)would enable Jetex and Rapier flyers in the western hemisphere to enjoy ourhobby with no worries about being unable to obtain jet motors for ourmodels. Could anyone here suggest propellant formulas for such low-thrust,long-burning jet motors?Sugar propellants are generally not suitable for end burners because it is difficult to get the burn rate fast enough for them to generate sufficient thrust -- at least for rocketry applications. However, I just attempted some simulations based on your requirements and it does seem theoretically possible to hit that ballpark. A 5mm diameter grain (about the smallest you want to work with) will produce about 3/10 N, and 40mm length will provide a 5.4 second burn time. Total impulse is 1.68 Ns, 42% A. -p. ----- No virus found in this message. Checked by AVG - www.avg.com Version: 10.0.1432 / Virus Database: 3658/6465 - Release Date: 12/31/13