Sciencemadness Discussion Board

Energetic binders

DubaiAmateurRocketry - 5-11-2013 at 08:22

First this site need an auto-save thing, I miss clicked something and it all went gone, so annoying.. Anyways..

I realized there are almost little discussion about energetic binders, so I thought I want to start one.

Binders often decrease performance significantly, however these ones, are not too expensive, and I personally most look forward to the energetic BAMO for propellants, BNMO for binder bonded explosives, and Nitrated--HTPB for properties.

Here are their structures




Here are some papers I saved on my computer.

Energetic binder, plasticizer systems.

Compatibility between GAP and HTPB
http://sci-hub.org/pdfcache/071d8d5d23a853352d5c211afcf576dc...

Good idea ! Hydroxyl diazodotriazene terminated poly butadiene.
http://www.ias.ac.in/matersci/bmsjul2011/745.pdf

Well written and informative. Synthesis and thermal decomposition of GAP and Poly(BAMO) copolymer
http://libgen.org/scimag2/10.1016/j.polymdegradstab.2007.03....

Alkaabi synthesis -
Well written and informative. GAP, GTP complete guide
GAP Glycidyl Azide Polymer + HT-GAP (Hydroxyl terminated Glycidyl Azide Polymer) + other nitrogenous polymer.
https://www.google.ae/url?sa=t&rct=j&q=&esrc=s&a...

Recent trends in Enegetic polymers and plasticizers
1. http://www.dtic.mil/dtic/tr/fulltext/u2/a377866.pdf

2. http://www.dsto.defence.gov.au/publications/2210/DSTO-TR-096...

3.http://www.smf.phy.cam.ac.uk/fsp/Publications/Energetics%20papers/211EMAgrawalPECS24.pdf

List of azide, nitrated plasticizers. Well written.
http://libgen.org/scimag4/10.1134/S207997801203003X.pdf

Direct conversion of epichlorohydrin to glycidyl azide polymer
https://docs.google.com/viewer?url=patentimages.storage.goog...

Heat of formation of some Azide containing Oxetane
Monomers and Polymers
https://e-reports-ext.llnl.gov/pdf/244050.pdf

Azide terminated azido compounds for plasticizer.
https://docs.google.com/viewer?url=patentimages.storage.goog...

Diisocyanate terminated azido compounds.
https://docs.google.com/viewer?url=patentimages.storage.goog...

An azide terminated GAP useful plasticizer
https://docs.google.com/viewer?url=patentimages.storage.goog...

Hydroxyl terminated GAP
http://worldwide.espacenet.com/publicationDetails/originalDo...

HT-azide containign polyers.
https://docs.google.com/viewer?url=patentimages.storage.goog...

Poly-BAMO copolymers
http://www.jatm.com.br/papers/vol2_n3/JATMv2n3_p307-322_Synt...

Poly-BAMO + Poly-AMMO characteristics
http://onlinelibrary.wiley.com/doi/10.1002/prep.200600054/pd...

NCO-(CH2)6-[GAP]n-(CH2)6-NCO isocyanate functional GAP !
https://docs.google.com/viewer?url=patentimages.storage.goog...

nitrated compounds with isocyanates.
https://docs.google.com/viewer?url=patentimages.storage.goog...

Nitrated HTPB - NHTPB
https://attachment.fbsbx.com/file_download.php?id=1420082624...

Advanced propellant chemistry-Gould R.F.-
http://www.libgen.net/view.php?id=853382

Energetics binders, book.
http://books.google.ae/books?id=ykVXPCaiRtYC&pg=PA27&...

underground - 5-11-2013 at 12:38

Something easy to manufacture, with common materials ? And as less toxic as possible? I am also interested in cause of the rocketry theme, not only about the HE

Maybe we could also find a good comp for AN based propellants with those binders...

DubaiAmateurRocketry - 6-11-2013 at 08:39

Quote: Originally posted by underground  
Something easy to manufacture, with common materials ? And as less toxic as possible? I am also interested in cause of the rocketry theme, not only about the HE

Maybe we could also find a good comp for AN based propellants with those binders...


AN is not energetic at all, at least AP to begin with. I want to find a stable tetrazole oxidizer.

and for binders, the N-HTPB and BNMO meets your requirements. NHPTB can be easily made in 2 steps from commerical HTPB you can buy from many suppliers since it is used in plastics.

NHTPB have a higher density, around 1.3, depending on the level of nitration.

the more nitration on HTPB, the mechanical properties goes down, the optimum is around 10% nitration, gives a good margin between oxygen balance, density, cost, and performance.

Fantasma4500 - 6-11-2013 at 10:13

when SHN (Sorbitol Hexa Nitrate) is succesfully nitrated (yeah good luck!! :D) a sirup of mixed nitrates is found, this is then redissolved in ethanol or other solvent and crystallized out by being poured into water..
i suppose the sirup COULD be used as a sort of plasticizer?? of what ive read it has significant use in the gunpowder propellants industry, probably even in military grade propellants aswell?

DubaiAmateurRocketry - 6-11-2013 at 10:33

Quote: Originally posted by Antiswat  
when SHN (Sorbitol Hexa Nitrate) is succesfully nitrated (yeah good luck!! :D) a sirup of mixed nitrates is found, this is then redissolved in ethanol or other solvent and crystallized out by being poured into water..
i suppose the sirup COULD be used as a sort of plasticizer?? of what ive read it has significant use in the gunpowder propellants industry, probably even in military grade propellants aswell?


I have read little about SHN, and I am not sure what the sirup, you're talking about, is.

for plasticizers, I have linked few papers on my post you can find.

NeonPulse - 7-11-2013 at 03:34

nice collection of papers there. ill be reading through some of them for sure the concept of energetic binders+plasticizers have always intrigued me.it always seemed counter productive to add a non energetic element to explosive, altering some of the more desirable properties they have thanks for posting the wealth of info. much apreciated. NP

Microtek - 7-11-2013 at 05:06

I'd like to disagree that AN is not suitable as a propellant base. I have experimented with an AN/silicone rubber/Al propellant which was extremely energetic. The idea (for me) came from a topic here on SM some years ago, but is really an old notion. I used phase stabilized AN and 3 um Al along with silicone rubber.
Later, I altered both the formulation and the procedure by including a granulated NC/NG propellant and dissolving the (un-hardened) silicone rubber in detergent gasoline, mixing in the other ingredients and evaporating the solvent under agitation. This gave a molding powder that I pressed into a motor case around a special coring tool with a "+" cross section (made in my hobbyist machine shop). Then I added a nozzle with a very small throat (steel).
These rockets (12 mm OD, 50 mm long) were fairly difficult to ignite (one reason I added the NC/NG was for greater ease of ignition) but once they were, they accelerated fast enough that I think you could use them as kinetic penetrators (like the gyro-jet).

DubaiAmateurRocketry - 7-11-2013 at 05:22

Quote: Originally posted by Microtek  
I'd like to disagree that AN is not suitable as a propellant base. I have experimented with an AN/silicone rubber/Al propellant which was extremely energetic. The idea (for me) came from a topic here on SM some years ago, but is really an old notion. I used phase stabilized AN and 3 um Al along with silicone rubber.
Later, I altered both the formulation and the procedure by including a granulated NC/NG propellant and dissolving the (un-hardened) silicone rubber in detergent gasoline, mixing in the other ingredients and evaporating the solvent under agitation. This gave a molding powder that I pressed into a motor case around a special coring tool with a "+" cross section (made in my hobbyist machine shop). Then I added a nozzle with a very small throat (steel).
These rockets (12 mm OD, 50 mm long) were fairly difficult to ignite (one reason I added the NC/NG was for greater ease of ignition) but once they were, they accelerated fast enough that I think you could use them as kinetic penetrators (like the gyro-jet).


AN compared to old old fuels like black powder, yes it then is energetic since it produce a lot of gas. However... It has a very low density, just above 1.7.

Its decomposition is also not as exothermic as ammonium perchlorate, It can not even burn with polyurethane without the addition of magnesium, titanium, or maybe silicone since it worked for you. Even aluminum does not combust with ammonium nitrate without energetic binders.





This is AP vs AN. and ANCP are very oxygen negative and also much less dense than APCP.

Dany - 7-11-2013 at 05:57

@DubaiAmateurRocketry

Microteck replied to your statement that ammonium nitrate is not energetic at all. Now AN is not as performant as AP, yes we all agree. However, and based on the graph that you just post, i see that AN propellant composition (based on specific impulse) are interesting for an amateur. for example, an Isp of 238 s for 62% AN-20%Mg-18%R45 (@ 1000 psi) is not too low compared to high performance AP composition. Also, AN is far less expensive than AP.

Dany.

DubaiAmateurRocketry - 7-11-2013 at 06:12

@Dany

Hey I apologize for any exaggerations, but I said that while replying to underground.

Underground:
Quote:

Maybe we could also find a good comp for AN based propellants with those binders...


I said that because AP is not expensive nor hard to find, so using AN on these expensive binders which take hours or days to make, is kind of a waste.


Finally, AN IS actually a bad oxidizer for rocket fuels. It has one of the slowest burn rates and only a moderate combustion temperature. It is also uncompatible with many fuels, mixtures of AN with Sugar, PU, HTPB, hexamine can not even ignite.

malford - 7-11-2013 at 07:42

Excerpt from one of the papers below. Can someone explain what ecombn kcal/mol is?

Density -- kcal/mol -- ecombn kcal/mol -- OB -- Tg C

Nitroglycerine (NG)
1.60 –83.97 368.4 +3.5 –68

Diethyleneglycol bis(azidoacetate)
(DEGBAA)
1.00 –329 1081.07 –100 –63.3

Trimethylolnitromethane(triazidoace
tate) (TMNTA)
1.45 –230 1294.04 –72 –34.1

Pentaerythritol tetrakis(azidoacetate)
(PETKAA)
1.39 –215 1714.76 –89 –35.4

Dany - 7-11-2013 at 08:23

Quote: Originally posted by malford  
Excerpt from one of the papers below. Can someone explain what ecombn kcal/mol is?


??

DubaiAmateurRocketry - 7-11-2013 at 10:39

Quote: Originally posted by malford  
Excerpt from one of the papers below. Can someone explain what ecombn kcal/mol is?


Although im not sure what is the ecombn, maybe it shows how much heat is given off when it is completely burned ? or decompose ? I am not sure.

Any ways, what do you guys think are most promising ? The Nitrated HTPB is also miscible with all polar liquids, which means, finally, these energetic plasticizers can be mixed into NHTPB which i think is not hard to produce on industrial scale.

Ethyleneglycol bis(idoacetate) (EGBAA)
Density 1.34
HOF –167.36
HOC 796.26
OB –84.15
Tg –70.8

Tg -71 is amazing, and it has a good density, however the more traditional DTTN, although with higher Tg, is more cheap to produce, and ... it has a much higher density 1.5(in paper) or a lower density 1.2(wikipedia). If its 1.5, I think DTTN would need no replacement. I think the wikipedia one is wrong.

malford - 7-11-2013 at 11:19

Dany, perhaps I worded my statement in a confusing manner. I meant, below was an excerpt from one of the papers in the original post. I selected those compounds because they had the highest kcal/mol from one of the charts in the paper to which I linked. That chart has two columns, one for kcal/mol and another for ecombn kcal/mol. I don't know what ecombn kcal/mol is and was hoping someone could tell me.

DubaiAmateurRocketry, EGBAA has a high HOF, but DEGBAA is significantly higher. Compare -167 to -329. If I had more free time right now, I'd find more information about these compounds and build a chart which shows kJ/cm3. I believe comparison based on volume is more beneficial because rocket motors and their igniters will be limited by volume not weight.

DubaiAmateurRocketry - 7-11-2013 at 11:24

Quote: Originally posted by malford  

DubaiAmateurRocketry, EGBAA has a high HOF, but DEGBAA is significantly higher. Compare -167 to -329. If I had more free time right now, I'd find more information about these compounds and build a chart which shows kJ/cm3. I believe comparison based on volume is more beneficial because rocket motors and their igniters will be limited by volume not weight.


Umm, do you mean lower ? Its negative so the smaller the number the larger.

So EGBAA > DEGBAA in HOF, Density, and Tg.

Dany - 7-11-2013 at 12:00

Quote: Originally posted by malford  
Dany, perhaps I worded my statement in a confusing manner. I meant, below was an excerpt from one of the papers in the original post. I selected those compounds because they had the highest kcal/mol from one of the charts in the paper to which I linked. That chart has two columns, one for kcal/mol and another for ecombn kcal/mol. I don't know what ecombn kcal/mol is and was hoping someone could tell me.


well, first it is Ecombn and not ecombn. What the authors mean by that is the Energy or heat of combustion. So the heat of combustion of nitroglycerine is Ecombn= 368.4 kcal/mol.

Dany.

malford - 7-11-2013 at 12:39

Quote: Originally posted by Dany  
Quote: Originally posted by malford  
Dany, perhaps I worded my statement in a confusing manner. I meant, below was an excerpt from one of the papers in the original post. I selected those compounds because they had the highest kcal/mol from one of the charts in the paper to which I linked. That chart has two columns, one for kcal/mol and another for ecombn kcal/mol. I don't know what ecombn kcal/mol is and was hoping someone could tell me.


well, first it is Ecombn and not ecombn. What the authors mean by that is the Energy or heat of combustion. So the heat of combustion of nitroglycerine is Ecombn= 368.4 kcal/mol.

Dany.


Thank you, Dany, for pointing that out. Since heat of combustion is defined as the difference between the heat of formation of the products and reactants, and since these compounds consist of homogenous molecules rather than mixtures of fuel and oxidizer, how, then, is the heat of combustion not the same as the inverse of the heat of formation? I am strictly referring to the compounds in the chart in the aforementioned paper.

Also, Dany, I'd like to return the critical favor. The beginning of your post should be capitalized. You should have used "Well" instead of "well". Also, you are missing a comma after "So". It should look like "So, the heat...". Lastly, your signature, currently "Dany." aspires to be what is known as a sentence in the body of rules called English grammar by displaying the period. It, sadly, falls short. "Dany" would be more appropriate.

Have a nice day.

Dany - 7-11-2013 at 13:15

with or without capitalization, with or without comma, at least you are understanding what is written. However, we will spend all the day to understand ecombn. Here, we are on a science forum so the most important thing is the scientific language. Grammar and poetry is secondary. Sadly, a lazy person put ecombn instead of Ecombn...

Back to your question: heat of formation and heat of combustion are different.

"Heat of formation is the is the heat of reaction or enthalpy change involved in making a particular compound, or molecule, from its elements where both the elements and compound are at standard-state condition" for more information see Explosive engineering for Paul W.Cooper.

"The heat of combustion of a specified substance is the heat
evolved when it is converted to the standard oxidation products
by means of molecular oxygen" see M.H. Keshavarz et al. / Journal of Hazardous Materials 185 (2011) 1086–1106 (and reference therein).

Dany.

[Edited on 7-11-2013 by Dany]

woelen - 8-11-2013 at 01:15

I moved some offtopic drivel to detritus. Please stay on topic and stop derailing the thread.

malford - 8-11-2013 at 04:46

woelen, I appreciate your fervor for keeping the information on the forum relevant and useful. I actually took the time to go to detritus and see what was moved and found only the image I had posted. You may not have read the image and understood the purpose of it. The point of the image is not made out of the context of this thread. For your convenience, I will show it again in this post which is now on topic and contains further contribution below to the thread's OP. Also, if you'd like to clean up off-topic bickering, all of the posts regarding AN are entirely unrelated.



Dany, I understand the definitions of the combustion enthalpy and formation enthalpy, but my question was specific to this list of compound which are not mixtures. How can combustion occur with homogenous compounds? Logically, I see the only route for combustion would be once the molecule decomposes, the decomposition products combust. If this is the case, I still don't see how the absolute value of enthalpy change of some decomposition products combusting would be larger than the total enthalpy change of the formation from elements.

[Edited on 8-11-2013 by malford]

[Edited on 8-11-2013 by malford]

Fantasma4500 - 8-11-2013 at 08:05

well, DubaiAmateurRocketry .. sorry for late reply..
the product you get from nitration is a mix of nitrates, which is somewhat oily and sticky, meaning you can stick this to a solid without making it worse as in properties..
ratios can be fixed..
if you want to have a rocketfuel thats OB and you dont wanna mess more with the OB you can make EGDN which has a PERFECT OB meaning you dont need to regulate oxidizer / fuel in the rocketfuel and can just add until you think its enough

Dany - 8-11-2013 at 15:51

Quote: Originally posted by malford  
Dany, I understand the definitions of the combustion enthalpy and formation enthalpy, but my question was specific to this list of compound which are not mixtures. How can combustion occur with homogenous compounds? Logically, I see the only route for combustion would be once the molecule decomposes, the decomposition products combust. If this is the case, I still don't see how the absolute value of enthalpy change of some decomposition products combusting would be larger than the total enthalpy change of the formation from elements.


As i explained above the "Heat of formation is the is the heat of reaction or enthalpy change involved in making a particular compound, or molecule, from its elements" since the heat of formation of the element is zero (e.g., carbon, Oxygen, fluorine, O2, F2...) so the heat of formation is the energy content of the molecule just formed, whereas the heat of combustion (when a molecule burn with O2 to form CO2, H2O...) is the heat difference between heat of formation of the products (CO2, H2O...which is not equal to zero) and the heat of formation of the compound which undergoes the combustion (e.g, TNT, a propellant...). This mean you can calculate the heat of formation if you know the heat of combustion (heat of formation and heat of combustion are not equal!). An example is illustrated in [1] page 644 where the authors determine the heat of formation of TNT from the known heat of combustion of TNT with oxygen, a reaction that yield CO2, H2O and N2. The heat of formation of CO2 and H2O are well known from thermochemical tables (see, http://webbook.nist.gov/chemistry/name-ser.html). Since we know the heat of combustion of the reaction (which is measured in a bomb calorimeter) the heat of formation of TNT= heat of combustion (of the reaction) minus heat of formation of reaction products. As you can see, heat of formation and heat of combustion are not equal.

a case where the heat of formation equal the heat of combustion [2] is the combustion of elements (e.g., C+O2----> CO2) since the heat of formation of carbon and oxygen (or other element like for example aluminum etc...) is equal to zero so here the heat of combustion is equal to the heat of formation of the products (in this case it is CO2)

[1] Chemistry and Physics of Energetic Materials, editor Surya N. Bulusu.
[2] Propellants and Explosives, Thermochemical Aspects of Combustion, Naminosuke Kubota (see page 280 under Heats of Combustion of Elements)

Dany.


DubaiAmateurRocketry - 17-11-2013 at 07:23

A method of curing azido-polymers where the amount of interlinked bonds can be controled.

This method of curing is also iso-cyanate free. It seems very interesting.


open file with adobe reader
Attachment: phpy4Z0DR (259kB)
This file has been downloaded 1968 times

[Edited on 17-11-2013 by DubaiAmateurRocketry]

DubaiAmateurRocketry - 10-12-2013 at 19:54

Interested by the reaction on page 68

https://smartech.gatech.edu/bitstream/handle/1853/7597/arons...

I think we can graft ''energetic'' tetrazoles onto GAP. This seems interesting !

Im not sure about if the mix acid will kick the tetrazole out and form Poly-GLYN or perform nitration on the COOH. and sorry for my bad drawing of polymers.




However this compound seems like it have a melting point at around room temperature with high viscousity and might not serve good as a ''binder'', however partial reactions still can be done to increase the density and oxygen balance.

If nitration fails, I really do think Trinitro-acetonenitrile can make the above compound. or polymer.

I have found little information about Trinitro-acetonenitrile however if it is a liquid and not a solid, and is compatible with some oxidizers and metal powders, it can be used to Cure GAP while giving oxygen balance during mixing ! making GAP propellant manufacturing crafting easier.

references for the above reaction.

Ralf Haiges * and Karl O. Christe Inorg. Chem., 2013, 52 May 31, 2013

and the paper i already posted.

[Edited on 11-12-2013 by DubaiAmateurRocketry]


[Edited on 11-12-2013 by DubaiAmateurRocketry]

[Edited on 11-12-2013 by DubaiAmateurRocketry]

roXefeller - 1-2-2014 at 07:33

Has any thought ever been given to a partial polymerization of glycerol, and then forming a nitrate ester with the remaining hydroxyl groups? Or would the nitrating split the oligomers apart to form NG?

DubaiAmateurRocketry - 1-2-2014 at 08:04

Quote: Originally posted by roXefeller  
Has any thought ever been given to a partial polymerization of glycerol, and then forming a nitrate ester with the remaining hydroxyl groups? Or would the nitrating split the oligomers apart to form NG?


Good thought however what will we link glycerol with ?

I think it is ok to call Poly-GLYN(poly-glycidol nitrate), poly-glycerol-nitrate, Nitration of glycidol and glycerol both give nitroglycerin, however, glycidol could be linked together in the reaction of the 2nd picture on this post.

http://www.sciencemadness.org/talk/viewthread.php?tid=28450

poly GLYN is just glycerin connected similar to how diethyleneglycol, tri-tetra, etc, is, however since it have an extra hydroxyl group, it could be nitrated, which is GLYN. And this is why i find poly-GLYN most potential, except its instability when cured with urethane linkages. My proposal on that post to solve the instability with urethane linkage also gives the problem of limited plasticizers since the curing is done with azido groups, any plasticizer containing the azido group most probably could not be used.

polyGLYN have a lot of advantages over GAP, such as significantly higher OB and density, and insensitive at the same time(Impact sensitivity >20J)

[Edited on 1-2-2014 by DubaiAmateurRocketry]

roXefeller - 1-2-2014 at 19:10

The polymerization with phthalic anhydride seems to be a common college-level reaction to form a polyester.

DubaiAmateurRocketry - 3-2-2014 at 10:20

Quote: Originally posted by roXefeller  
The polymerization with phthalic anhydride seems to be a common college-level reaction to form a polyester.


I dont think its more efficient than Poly-GLYN, would it even be a liquid ?

Edit: forgot to add ''dont'' in the sentence.

[Edited on 4-2-2014 by DubaiAmateurRocketry]

roXefeller - 3-2-2014 at 14:02

It does set up to a thermoset, but that's why I'm conjecturing about the partial polymerization. Since it uses equimolar amounts of phthalic anhydride and glycerol and it's not a catalyzed homopolymer, backing off the phthalic anhydride should keep it as soft oligomers.

franklyn - 6-2-2014 at 01:55

Modern high-energetic polymers

www.chemikinternational.com/pdf/2010/01_2010/chemik_01_2010_018_020.pdf

.

DubaiAmateurRocketry - 9-2-2014 at 10:35

I believe Poly glycidyl nitrate (aka PGN or poly-GLYN or GNP) Should be the future binder. This patent's method for preparing it is much more cost effective than methods used before and synthesizing GAP.

US patent 6362311
https://docs.google.com/viewer?url=patentimages.storage.goog...

Synthesis of GNP, and DTGNP.



This tells why Glycidyl nitrate polymer is better than GAP.



[Edited on 10-2-2014 by DubaiAmateurRocketry]

roXefeller - 9-2-2014 at 17:51

The butane diol was chosen because it forms a preinitiator complex with the BF3. But it was only one of many diols possible. Will ethylene glycol do similar? It was presented to cocatalyze oligomers in this patent (http://www.freepatentsonline.com/4409415.html). That substitution is also useful as it increases the nitrogen percent by reducing the size of the R group.

DubaiAmateurRocketry - 10-2-2014 at 05:10

Roxefeller, Theoretically yes, I am not sure why butane diol is used, but maybe it is more reactive on the terminal hydroxyl groups.

On your question on the increase in energy since the R is smaller for ethylene diol than butane diol, for a molecular weight of 2000 GAP, Ethylene diol GAP contains 41.15% Nitrogen, meanwhile butane diol GAP have 40.6% N. Small improvement but why not. Glyerol which forms trifunctional GAP is even more favorable since if makes more elastic and crosslinked binder.

btw i drew the polymer wrong and its fixed now

roXefeller - 10-2-2014 at 14:05

I thought we were talking about Poly GLYN...

The description paragraphs of the patent discuss polymerization in the diol/BF3 etherate as you detailed. The examples also use CaH2, examples 8&9. Have you eliminated this as unnecessary?

[Edited on 11-2-2014 by roXefeller]

DubaiAmateurRocketry - 11-2-2014 at 09:01

Quote: Originally posted by roXefeller  
I thought we were talking about Poly GLYN...

The description paragraphs of the patent discuss polymerization in the diol/BF3 etherate as you detailed. The examples also use CaH2, examples 8&9. Have you eliminated this as unnecessary?

[Edited on 11-2-2014 by roXefeller]


Oh, I thought you meant GAP since GAP's energy has to do with the nitrogen content, GLYN is the amount of oxygen.

Umm for the CaH2, they mentioned its use to stop the reaction, im pretty sure it is not a necessary step. Cold water can stop the reaction easily, when water is added, water is miscible with CH2Cl2 and the polymer or glycidyl nitrate is kicked out from the solution (Im pretty sure glycidyl nitrate have a very bad solubility in cold water).

Dany - 11-2-2014 at 13:08

Quote: Originally posted by DubaiAmateurRocketry  
water is miscible with CH2Cl2


Just a little correction, dichloromethane CH2Cl2 is not miscible in water. In fact CH2Cl2 is a common solvent for aqueous phase extraction in organic chemistry lab.

Dany.

DubaiAmateurRocketry - 11-2-2014 at 13:35

Quote: Originally posted by Dany  
Quote: Originally posted by DubaiAmateurRocketry  
water is miscible with CH2Cl2


Just a little correction, dichloromethane CH2Cl2 is not miscible in water. In fact CH2Cl2 is a common solvent for aqueous phase extraction in organic chemistry lab.

Dany.


Ah, i didnt know that!

Is it possible to have Poly glycidyl nitrate(PGN), the one I drew, to have GAP section terminated polymer? Maybe by polymerizing the glycidyl nitrate first, and then when the reaction is done, add glycidyl azide? How can we make sure most of the polymer's end have a GAP section?

roXefeller - 11-2-2014 at 14:54

Quote: Originally posted by DubaiAmateurRocketry  

Oh, I thought you meant GAP since GAP's energy has to do with the nitrogen content, GLYN is the amount of oxygen.



Yeah, that's where I was going (percent oxygen fixed to nitrogen), but I should've said it better.

The CaH2 is a dessicant, so it probably dehydrates the polymerization process since water forms by way of terminating hydrogens reacting with the hydroxyls of the diol's. It may in fact be necessary as a catalyst. Further it is one of the first additions in the examples, so it cannot logically be used to stop the reaction according to the patent description. However, it may be that its absence stops the process, e.g. by selecting a certain molar quantity, the MW of the oligomers can be planned from the beginning when the CaH2 plays out. Further I suspect that given the choice of dessicant (one that chemically reacts with vigor), one of similar scavenging qualities is needed (Ac2O vice H2SO4 or CaCl2 or other anyhydrous compounds) if CaH2 is not chosen.

Do you know what sort of viscosity the PGN has prior to curing? It's novel enough that I'm having a hard time finding numbers, only 'viscous liquid' as descriptor. Possibly the incorporation of a small fraction of glycerol with the diol could be used to tweak the viscosity by adding a third functional group to increase the branching polymerization.

[Edited on 12-2-2014 by roXefeller]

roXefeller - 24-2-2014 at 17:49

I had this wrong. I'm suprised I wasn't corrected. There isn't water being produced during polymerization, and it is purely a matter of Lewis acid catalysis of epoxide/hydroxyl additions. It does appear that water present would reduce the glycidyl nitrate to glycerol mononitrate, perhaps the reason for the CaH2 dessication. Ac2O would be damaging, reacting with the epoxide groups to form acetates. Somehow I thought that alternating units of epoxide and diol monomers were linked, so the use of glycerol is also mostly wrong. The polyol was just present to initiate the chain and provide hydroxyl for the first epoxide addition.

[Edited on 25-2-2014 by roXefeller]

DubaiAmateurRocketry - 25-2-2014 at 09:48

Quote: Originally posted by roXefeller  
I had this wrong. I'm suprised I wasn't corrected. There isn't water being produced during polymerization, and it is purely a matter of Lewis acid catalysis of epoxide/hydroxyl additions. It does appear that water present would reduce the glycidyl nitrate to glycerol mononitrate, perhaps the reason for the CaH2 dessication. Ac2O would be damaging, reacting with the epoxide groups to form acetates. Somehow I thought that alternating units of epoxide and diol monomers were linked, so the use of glycerol is also mostly wrong. The polyol was just present to initiate the chain and provide hydroxyl for the first epoxide addition.

[Edited on 25-2-2014 by roXefeller]


I dont think glycidyl nitrate + Ac2O = glycidyl acetate and nitric acid ? Will nitric acid really form?

I dont think glycidyl nitrate will not reduce glycidyl nitrate into glycidyl mononitrate because if you read examples of the patent on the synthesis of glycidyl nitrate, NaOH, CH2Cl2, and nitric acid, all are in solution. NaOH was a dilute 30%, and HNO3 was 90%.

So it means it shouldnt react with water.

If CaH2 is used for dehydration, they will put more than 1 gram on a 1.5 kg batch for example9.

roXefeller - 25-2-2014 at 15:04

I think the acetate doesn't form with the nitrate, but on the group formed when the epoxide opens. Wikipedia mentioned it in the oxirane article for reactions with anhyrides.

But the glycidyl nitrate was separated from the aqueous phase in the CH2Cl2. Then dried with MgSO4, filtered and evaporated. It is then mixed with new CH2Cl2 and CaH2 added. It should be anhydrous by that point. But given its reactivity with water to form glycerol mononitrate it will do its own water scavenging and then provide initiator sites after such. The process of glycidyl nitrate going to glycerol mononitrate looks like the same process as when ethylene oxide reacts with water to form ethylene glycol, and its a industrial process for such.

DubaiAmateurRocketry - 26-2-2014 at 11:27

Oh, I forgot that the NaOH in the solution will keep glycidyl nitrate's oxirane ring from opening, therefore it was alright for HNO3, CH2Cl2 to contain water. What you said should be right, however I still kind of disagree about the desiccant part. I have read a handful of papers about GAP and so on, and none of them used any desiccant? Even if CaH2 was used as desiccant, why 1 gram for such a big batch? GAP's synthesis is very similar except it is glycidyl azide.

Any ways, Ill try these one day. I am wondering how do I get chemicals when I move to the US...

[Edited on 26-2-2014 by DubaiAmateurRocketry]

roXefeller - 26-2-2014 at 12:18

These are very readily available in the states, at least for the nitrate version. The biggest hurdle will be nitric acid, BF3 etherate, and methylene chloride. But these can be managed. One thing that startled me today was browsing the nitromethane on Amazon. The 'also purchased by' list included ice packs, stirring rods, methanol, sulfuric acid, hexamine, aluminum powder, methylene chloride, etc. I can't believe the amount of data logging that is being done by merchants. It's dangerous.

DubaiAmateurRocketry - 3-4-2014 at 13:46

Just wow, This new paper published just last year has shortened the N2O5 synthesis of Nitro-HTPB into a single step NaNO2-I2 1 step synthesis with cheapest chemicals possible.

Unfortunately, the amount of nitro groups hanged onto the polymer backbone is not given, however the ease of synthesis is remarkable! NHTPB's important characteristic is low glass transition temperature(not much difference with HTPB), around 10-20% higher density, and finally the most important - miscibility with other energetic plasticizers which can help with the OB.

The paper is in the uploads.

https://docs.google.com/viewer?url=patentimages.storage.goog...

This patent shows another plasticizer found in this century, It's claimed to have a TC impact sensitivity of 117cm, and ABL impact sensitivity of 11cm. (I have no idea what is those 2 impact sensitivity measurements are.)

Judging from the structure, I feel this plasticizer should not be impact sensitive. It has yet to report its glass transition temperature but it require no more oxygen to burn it self, with an amazing density of 1.47. Its melting point is lower than -60 degree Celsius which is a good sign of a very good plasticizer.

Attachment: phpGT2PHo (703kB)
This file has been downloaded 1266 times
]

[Edited on 3-4-2014 by DubaiAmateurRocketry]

DubaiAmateurRocketry - 2-3-2017 at 13:13

interesting paper published the energetic materials journal in china.

This paper is about epoxy terminated - GYN, removing the initial problem of Glycidyl nitrate polymer's instability.

http://www.energetic-materials.org.cn/hncl/ch/reader/view_ab...

"The reaction between the end hydroxyl of poly(glycidyl nitrate)(PGN) and isocyanates is easily affected by ambient moisture, and the curing stability is poor. Aiming at these problems, epoxy-terminated poly(glycidyl nitrate) (e-PGN) was synthesized. Its structure was characterized by infrared spectroscopy(IR), nuclear magnetic resonance(NMR) and gel permeation chromotagraph(GPC), and its major physiochemical properties were tested. The main physical properties of e-PGN, such as glass transition temperature, viscosity, density, thermal decomposition temperature, were close to those of PGN. The curing reactions of e-PGN with epoxy curing agents, such as imidazole(IMD), o-phthalic anhydride(PA), n-ethylethylenediamine(NEED) and isophorone diamine (IPDA) were studied. Results show that the curing reaction of e-PGN with IMD, PA, NEED and IPDA at 60 ℃/70 ℃ can be performed. When PA is used as curing agent, the mechanical properties of the cured material outperformed; the tensile strength is 0.912 MPa, and the elongation at break is 354%. In addition, the mechanical properties of the cured samples stored at room temperature for 8 months remained almost unchanged."

PHILOU Zrealone - 7-3-2017 at 00:44

Quote: Originally posted by DubaiAmateurRocketry  
I believe Poly glycidyl nitrate (aka PGN or poly-GLYN or GNP) Should be the future binder. This patent's method for preparing it is much more cost effective than methods used before and synthesizing GAP.

US patent 6362311
https://docs.google.com/viewer?url=patentimages.storage.goog...

Synthesis of GNP, and DTGNP.

1jaxpc.jpg - 48kB

This tells why Glycidyl nitrate polymer is better than GAP.

2qvdu6g.jpg - 27kB

[Edited on 10-2-2014 by DubaiAmateurRocketry]

There is a problem with the reaction after the 4th Arrow...the butylen moeity R is lost...I don't see how the epoxide may form without splitting off the "polymer"...here it is no more an epoxide but an acetal because one carbon holds 2 oxygen (ether linkage), a H atom and a link to another C...

[Edited on 7-3-2017 by PHILOU Zrealone]

PHILOU Zrealone - 7-3-2017 at 00:56

Quote: Originally posted by DubaiAmateurRocketry  
Even aluminum does not combust with ammonium nitrate without energetic binders.


Belive me it does burn with dry ammonium nitrate especially when hyper-reactive ultrafine dendritic Al powder with low oxyd layer is used...

I have experimented with it--> It burns bright spreading star sparks all arround like a sparkler but fiercely and this from the simple flame of a cigaret lighter .

Laboratory of Liptakov - 7-3-2017 at 01:08

After reading this thread it seems, respectively I estimate, that will the miracle, if we sometime see only one gram the modern active binder - plasticizer. From preparations in amateur conditions........:cool:...Dr.

PHILOU Zrealone - 7-3-2017 at 01:18

Quote: Originally posted by DubaiAmateurRocketry  

Im not sure about if the mix acid will kick the tetrazole out and form Poly-GLYN or perform nitration on the COOH.

It is not the -CO2H that is nitrated but the CH2 between the two EWG (electron withdrawing groups) N#C- and -C(=O)-OH...

The Hs from the CH2 are thus more acidic and exchange easier for a N=O(+) or a NO2(+)...

EWG1-CH2-EWG2 + Y(+) --> EWG1-CHY-EWG2 + H(+)
If the Y is N=O it can take the oxime form..
CH-N=O <==> C=N-OH
If the Y is NO2 it is also a stonger EGW and allows for easy (spontaneous?) decarboxylation of the -CO2H into -H + CO2
You thus get EWG1-CH2-NO2 and the Hs are even more acidic and prone to be attacked by an extra NO2 thus leading to EWG1-CH(-NO2)2 itself even more reactive and leading to EWG1-C(NO2)3...

Into the case Y is equal to -N=O maybe decarboxylation occurs also (first?)or it goes via oxydation of the C-N=O into C-NO2 and then it decarboxylate like in the previous exposed case Y=NO2...
But further NO(+) attacks the EWG1-CH2-NO2 and makes a nitrolic acid (nitrosonitromethylene) what is not oxidized further into a dinitromethyl-, a dinitronitrosomethyl or trinitromethyl- group.
EWG1-CH2-NO2 + N=O(+) <--==> EWG1-CH(-NO2)-N=O + H(+)
EWG1-CH(-NO2)-N=O <==> EWG1-C(-NO2)=N-OH


[Edited on 7-3-2017 by PHILOU Zrealone]

PHILOU Zrealone - 7-3-2017 at 01:25

Quote: Originally posted by Laboratory of Liptakov  
After reading this thread it seems, respectively I estimate, that will the miracle, if we sometime see only one gram the modern active binder - plasticizer. From preparations in amateur conditions........:cool:...Dr.

May be hard for those exposed into the tread but not impossible...

There are indeed many potentially explosive polymers or explosives that could be used alone or in composite mix (to adapt to the requirements of the use as binders, as crosslinking reagents (curing) or as plasticizers...)

Don't forget that after all nitrocellulose and most of its propellant mixes (double base, single base) are of that kind...and NC is pretty amateur-ish ;-)

DubaiAmateurRocketry - 7-3-2017 at 09:26

About the the butylen R being lost was a drawing error, instead of trying to draw the entire structure I used a picture from an article.


Quote: Originally posted by Laboratory of Liptakov  
After reading this thread it seems, respectively I estimate, that will the miracle, if we sometime see only one gram the modern active binder - plasticizer. From preparations in amateur conditions........:cool:...Dr.


Yeah, I'd definitely want synthesize some, however not anytime soon - until I can test it with other oxidizers. Which will be few years as college has been pretty busy.

MineMan - 2-3-2019 at 13:51

All a few questions. How do you cure these energetic binders...? I would like to make cast propellant but the only way I can think of is acetone and Nitro cotton... but I don’t I could get the acetone to evaporate...

I am assuming cures are always used for rocketry and PBX?

Has anyone tried these energetic binders? How do you cure them??

Simoski - 1-4-2019 at 10:19

I watched a Laboratory of Liptakov YouTube video where he immerses a roll of insulation tape into petroleum for a few days, then removing the tape he has the sticky stuff dissolved in the petroleum .

He goes on to plasticize various energetics with it.

The sticky stuff is Pib, Polyisobutylene.

I do not know if this will help but I would take the fuel and oxidiser, mix it together with the petroleum/Pib and let the petroleum evaporate away. Should leave a plasticized grain.

Herr Haber - 1-4-2019 at 11:28

Are you suggesting you would use an unknown quantity of PIB ? :o

I'm kidding but that's a good reason. If it's not reproducible...

Laboratory of Liptakov - 1-4-2019 at 11:54

MineMan meant an energetically active binder. Such as nitrocellulose, or something else - nitro - that is itself active without further, major propellant. That's why I didn't suggest PIB or anything else that isn't an active binder. Of course that exist active binder, this is diethylenglycol dinitrate (DEGDN) mixed with nitrocellulose. Arises solid rocket fuel: https://en.wikipedia.org/wiki/Diethylene_glycol_dinitrate
However, modern best propellant are ammonium perchlorate + alu powder as main fuel + epoxy as super solid binder as secondary fuel in one.

MineMan - 1-4-2019 at 22:34

LL. Yes. Energetic bind is much better than epoxy... for explosives at least. As it allows metal powders to react quickly.

Microtek - 2-4-2019 at 01:08

For rocket propellant grains (AN/Al based), I have used an NG/NC binder system as follows:

- Powdered NC was mixed with NG in a 50:50 ratio by dissolving NG in enough ethanol to wet the powdered NC

- Then the other components were mixed in and the ethanol was allowed to evaporate

- Finally, the propellant was pressed into the mold with a dwell time of about 5-10 minutes. This allows the NC/NG granules to flow into each other and form a rubbery matrix (much like a sintering process)

It only works well at relatively high NG/NC ratios, and does require pressing.

MineMan - 3-4-2019 at 23:43

You made a propellant with AN/Al!? Tell us more!!

For a big rocket this would be a lot of nitroglycerine, which I don’t feel safe with... I take it nitromethane or something safer could not be used because of the evaporation.

Or is nitroglycerine really not dangerous... only handled it once... use to handling solids.

XeonTheMGPony - 4-4-2019 at 05:06

Quote: Originally posted by MineMan  
You made a propellant with AN/Al!? Tell us more!!

For a big rocket this would be a lot of nitroglycerine, which I don’t feel safe with... I take it nitromethane or something safer could not be used because of the evaporation.

Or is nitroglycerine really not dangerous... only handled it once... use to handling solids.


Well cleaned samples are as safe as any other energetic, I have had a pure 1cc sample now in a syringe for over a couple years and I test it every so oft.

I am speaking of small scale batch sizes, and good handling protocols, once it is made, and cleaned dissolve it in the solvent of choice.

Have a clean bench with only the things needed for the job and line with paper mat to absorb any drips.

Nitrosio - 24-4-2020 at 07:24

http://pyrobin.com/files/Polymere%20Sprengstoffe.pdf