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Author: Subject: powdered Zn
chemrox
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[*] posted on 19-1-2007 at 00:21
powdered Zn


Back in the day, I made rocket fuels and pipe bombs with mixtures of powdered Zn & Sulfur flowers.

How would Zn stack up against Al in some of the mixes here?

My inorganic consists of point groups & symmetry
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quicksilver
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[*] posted on 19-1-2007 at 06:19


In what context do you mean "stack up"? - As a "fuel to fuel" basis the comparison would need to take into account size shape and purity of the particle matter from both groups then if you were just talking about oxidizer/fuel type stuff....



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[*] posted on 19-1-2007 at 06:31


I just tried it and it did nothing beyond just burn the sulpher off?
10micron alu and RG sulpher powder.




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[*] posted on 19-1-2007 at 06:39


Aluminum is nice and chemically resistant to some things.

I've never had aluminum (filings) burn in thermite until rather high temperatures were reached.




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[*] posted on 19-1-2007 at 06:48


well I was introduced to S/Zn as a rocket fuel when I was much, much younger and it works but you need to compress it, etc.....compair it to KNO3 and suger or BP and the later have a faster burn rate. IF WE ARE TALKING ABOUT ROCKETS... Sulfur and zinc has some push which was valued - however faster burn rate wasn't always the objective in a launch. Back then the best for speed of burn that I used to work with was ammouium perchlorate and aluminum flake in a polymer pellet (formed in rocket tooling, bla, bla) THAT was very powerful -=and=- fast for larger sized motors. The big ones that guys used to make in the club I used to be in were almost military sized and astounding in what they could do. Once, a club in Phoenix AZ had to get in touch with the FAA before a launch due to size and flight considerations! (NO bullshit!) That thing was the size of a Tomahawk and flew like nothing I had seen before. That was when they first started using altimeters and various electronics. Today they use them on most rockets due to recovery efforts of the clubs involved (mucho dollars spent now-a-days)...:D Hell, I don't even know if we are talking about rockets - I just interjected it as S/Zn was a rocket fuel that I used.



[Edited on 19-1-2007 by quicksilver]




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[*] posted on 19-1-2007 at 07:14


well I only made about 100mg, as I had no idea if it flash off or something unpredictable. maybe that`s why? I used a mini blowtorch to light it, the sulpher burned great :)

I must admit, I did expect it to do Something more than it did :)




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[*] posted on 20-1-2007 at 19:10
Powdered Zn


I've experimented with various rocket fuels including Zn/S. I added red gum to the Zn/S and then acetone to dissolve the red gum. Upon loading into the rocket motor and allowing to dry (evaporate the acetone) I had a very compact, strong cylinder of rocket fuel that never CATO'd.



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[*] posted on 5-1-2008 at 17:11


In what ratio should Zn and S be mixed?



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[*] posted on 5-1-2008 at 17:30


Quote:
Originally posted by Zinc
In what ratio should Zn and S be mixed?


If you don't know that you probably shouldn't be mixing them....:(

Zn + S ---> ZnS

1 mole Zn + 1 mole S ---> 1 mole ZnS

65.37g + 32.06g ---> 97.43g

So roughly 2 parts Zn to 1 part S by weight.
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[*] posted on 6-1-2008 at 12:50


The ratios of S and Zn can be calculated as Xenoid did in the previous post, BUT, the best thrust may not be from that exact ratio. The rate of burning and the temperature of the exhaust 'gas' may be tilted to a more favorable direction by changing it. For example a little more Sulfur may not be needed to completely balance the Zinc, but it may speed up the reaction and provide a quicker burning with easier ignition and better thrust. It may provide a better bond for grain formation and as a gas that can be heated up and ejected at a higher speed. Part of the fun of rocketry was the experimentation with these small changes, and figuring out why.
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[*] posted on 6-1-2008 at 13:04


Xenoid I knew that it can be calculated that way. Mr.Wizards posts explains why I asked.



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[*] posted on 6-1-2008 at 22:26


I believe the normal ratios are normally quite close to stoichiometric. My notes show a ratio of 67 zinc to 33 sulfur as pretty common. Pretty much 2:1 I also have something about the addition of 10% potassium nitrate was said to give a little more zip to the rockets. I'm not sure if this is 10% additional, or if it replaces the zinc or sulfur. While zinc uses sulfur as an oxidiser, the potassium nitrate would be able to use it as a fuel, both chemicals actually. I never experimented much with these, so these are notes I took from reading/hearing accounts from others.
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[*] posted on 11-1-2008 at 12:50


CATO's in rockets is almost always traced back to inconsistent packing. That's why the hobbyists started packing with automobile jacks and developed super heavy compression (without impact, of course). You can do some wild experiments with the right tools for construction. The perchlorate / Al fuel was perhaps the strongest thing I personally saw. But there are guys who make black powder rockets that can push 2-4 lbs of stuff up to 6,000 ft. It just depends on what you want to spend. But the minute you have cracks or air pockets in the motor, all but the slowest thrusting motors will suck. I saw a sugar-KNO3 rocket that was made from PVC pipe, that even painted day-glow red went out of sight before you could follow it with the human eye. That's why before we had (or could afford) altimeters, we made them pop at the height of their flight; so we could see how high we got!



[Edited on 11-1-2008 by quicksilver]
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