Energetic triazolium salts

6509473
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Inventors

Drake, Greg W.

Application #

688909

Filed

Oct-16-2000

Published

Jan-21-2003

Current US Class

149/92
548/262.2
548/264.8
548/265.2
548/265.6

International Classes

C07D 249/08; C07D 249/14; C06B 025/34

Field of Search

548/262.2 548/264.8 548/265.2 548/265.6 149/92

Assignee

The United States of America as represented by the Secretary of the Air (Washington, DC)

Examiners

Ramsuer; Robert W.

Attorney, Agent or Firm

Stover; Thomas C.

US Patent References

5099028   Process for the synt...
5198204   Method of forming...
5254324   Dinitramide salts a...
5256792   Amine salts of nitro...
5274105   Hydroxylammoniu...
5472647   Method for prepari...
5684269   Hydroxylammoniu...
5847315   Solid solution vehic...

Referenced by:

View Backward References

Other References

V.I. Sloveetskii et al, Khim. Geter. Soedn. 1966, 2, 448-452. (Russian authors). G. Child, J. Heterocycl. Chem. 1965, 2, 98.

Citation

Cite This Patent

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Abstract
New energetic salts of 1,2,4-triazole; 3,4,5-triamino-1,2,4-triazole and of 4-amino 1,2,4-triazole were synthesized, characterized and their thermal and safety properties evaluated as possible new propellant ingredients. Energetic anions, including the nitrate anion, NO.sub.3, the perchlorate anion, ClO.sub.4, & the dinitramide anion, N(NO.sub.2).sub.2, were paired with the protonated heterocycles through facile, high yield synthetic routes to give crystalline, energetic salts. Using such a heterocycle system, either 1,2,4-triazole; 3,4,5-triamino-1,2,4-triazole or 4-amino 1,2,4-triazole, a new family of salts were synthesized through the direct reaction of the heterocycle with the corresponding acid form of the desired anion. These reactions were carried out in commonly available polar solvents, and at ambient temperatures, to give high purity, high yield products. All of the salts which were synthesized, were put through thermal stability tests and through impact testing, to reveal a robust family of new insensitive materials, suitable as new energetic propellant ingredients.
 
Claims
What is claimed is:

1. A method for making energetic triazole salts comprising, reacting the following: ##STR7##

where R and R' are H or NH.sub.2, except that when R'=H, R=H; and X.sup.- is NO.sub.3.sup.- ; ClO.sub.4.sup.- ; or N(NO.sub.2).sub.2.sup.-.

2. The method of claim 1 wherein: ##STR8##

3. The method of claim 1 wherein: ##STR9##

4. The method of claim 1 wherein: ##STR10##

5. A triazole salt of the formula: ##STR11##

where R and R' are H or NH.sub.2, except that when R'=H, R=H; and X.sup.- is NO.sub.3.sup.-, ClO.sub.4.sup.-, or N(NO.sub.2).sub.2.sup.-.

6. A triazole salt of the formula: ##STR12##

where X.sup.- is as stated in claim 5.



Description
RELATED APPLICATIONS

NONE

FIELD OF THE INVENTION

This invention relates to methods of preparation of energetic salts, particularly of triazole (or triazolium) salts and the resulting salts.

BACKGROUND OF THE INVENTION

Presently, hydrazine is used in propellant scenarios, whether as a boost material or in altitude control devices. Hydrazine has several shortcomings, most which are inherent to the basic properties of the material. It has a relatively high vapor pressure at ambient temperature, 12-14 torr, which leads to vapor toxicological problems, and is also a known carcinogen. Its specific gravity is approximately 1.0 g/cm.sup.3 at ambient temperatures. All of these properties can be significantly improved upon, with the use of new materials in monopropellant formulations.

In the prior art are U.S. Pat. Nos. 5,274,105 and 5,256,792, which disclose new energetic salts of high nitrogen heterocycles based on 1,2,4-triazole. But none are seen as pertinent to the claimed compositions.
 
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