Triaminoguanidinium phosphate propellant additive

4472214
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Inventors

Flanagan, Joseph E.
Grant, Louis R.

Application #

530325

Filed

Sep-8-1983

Published

Sep-18-1984

Current US Class

149/19.1
149/19.6
149/36
149/92

International Classes

C06B 045/10

Field of Search

149/19.1 149/19.6 149/92 149/36

Assignee

Rockwell International Corporation (El Segundo, CA)

Examiners

Miller; Edward A.

Attorney, Agent or Firm

Hamann; H. Fredrick, Field; Harry B.

US Patent References

3954528   Solid gas generatin...
4002514   Nitrocellulose prop...
4092188   Nitramine propella...

Referenced by:

View Backward References

Other References

Keim et al., J. Am. Chem. Soc., 72, 4944-4946 (1950).

Citation

Cite This Patent

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Abstract
Triaminoguanidinium phosphate is used to improve the performance and flammability characteristics of low vulnerability propellants.
 
Claims
What is claimed and desired to be secured by Letters Patent of the United States is:

1. A low vulnerability propellant having improved performance and flammability characteristics comprising a binder, cyclotetramethylene tetranitramine oxidizer, and from about 2.5 to about 15 weight percent of triaminoguanidinium salt of phosphoric acid.

2. A propellant of claim 1 wherein said triaminoguanidinium salt of phosphoric acid is from about 5 to about 10 weight percent of said propellant.

3. The propellant of claim 1 wherein said propellant is a gun propellant.

4. The propellant of claim 1 wherein said propellant is a rocket propellant.

5. The propellant of claim 1 wherein said binder is a copolymer of ethylene oxide and propylene oxide.



Description
BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention pertains to pyrotechnics and more specifically to propellant additives.

2. Description of the Prior Art

From U.S. Pat. Nos. 4,113,775 and 3,950,421 there are given processes for the preparation of bis-triaminoguanidinium tetranitroethane and triaminoguanidinium nitrate, respectively. The former compound is a strong oxidizer in a solid propellant composition, whereas the latter material is a key ingredient in gun propellant formulations. However, in the gun propellant area, there is now an effort to alter the composition of the propellant such that accidental ignition is avoided. Thus, it would be desirable to include in gun propellants a triaminoguanidinium compound containing a less oxidizing anion, if such exists, since it would be less energetic than the ones cited above. A strong candidate for this intended purpose would be a triaminoguanidinium salt of phosphoric acid. Unfortunately, no such triaminoguanidinium salt was known in the prior art.
 
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