Gas generant propellants

4358327
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Inventors

Reed, Jr., Russell
Lee, Benjamin Y. S.
Henry, Ronald A.

Application #

196893

Filed

Oct-14-1980

Published

Nov-9-1982

Current US Class

149/19.4
149/19.6
149/88
149/92

International Classes

C06B 015/10

Field of Search

149/19.4 149/19.6 149/92 149/88

Assignee

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

Examiners

Lechert, Jr.; Stephen J.

Attorney, Agent or Firm

Beers; R. F., Skeer; W. T.

US Patent References

4013596   Adhesive tetrazole...
4201853   Polymeric binders...

Referenced by:

View Backward References

Citation

Cite This Patent

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Abstract
A gas generant propellant composition having low flame temperatures comprng (a) an elastomeric binder consisting of a mixture of polyethylene capped polypropylene glycol and a dihydroxy tetrazole selected from the group having the formulas: ##STR1## (b) a curative agent such as the biuret trimer of hexamethylene diisocyanate; (c) a plasticizer agent such as 1-methyl-5 (methoxyethyl) tetrazole; (d) a coolant agent such as oxamide; and (e) a deflagrating agent selected from the group consisting of: dihydrazinium 3,6-bis(5-tetrazolyl)-1,2-dihydrotetrazine, dinitrosopentamethylenetetramine, the reaction product of glyoxal and hydrazine and the ammonium salt of 5-nitramino tetrazole.
 
Claims
What is claimed is:

1. A gas generant propellant containing:

A. a mixture of (1) polyethylene capped polypropylene glycol and a dihydroxy tetrazole selected from the group having the formulas: ##STR3## which has been cured by means of a diisocyanate; B. a plasticizer; and

C. a deflagrating agent selected from the group consisting of:

dihydrazinium 3,6-bis(5-tetrazolyl)-1,2-dihydrotetrazine, dinitrosopentamethylenetetramine, the reaction product of glyoxal and hydrazine and the ammonium salt of 5-nitramino tetrazole.

2. A gas generant propellant according to claim 1 which contains, in addition to the components set forth in claim 1, an oxamide coolant agent.



Description
BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to gas generant propellant compositions. More particularly, it relates to gas generant propellant compositions which are sufficiently cool to inflate various rubber and plastic devices. Still more particularly, this invention relates to gas generant propellants and a process for their preparation using high nitrogen compounds in which said high nitrogen compounds are used to sustain deflagration wherein a minimum of oxidizer is used and nitrogen is the major gaseous product.

2. Description of the Prior Art

A need exists for gas generant propellants which are sufficiently cool to inflate various rubber and plastic devices. Most gas generant propellants available have flame temperatures above 1800.degree. F. and pyrolyze the organic materials used in the manufacture of such inflatable devices. Thus, most propellants are not suitable for use therewith.

Conventional propellants contain a binder, which acts as a fuel and an oxidizer. Upon oxidation of the binder, deflagration occurs and the heat liberated by the formation of water and carbon dioxide produces relatively high flame temperatures. Attempts have been made to lower deflagration temperatures by limiting the amount of oxidizer used. However, when the oxidizer levels of a conventional oxidizer are reduced to achieve a flame temperature of a calculated acceptable value (in the range of about 1000.degree. F. to about 1200.degree. F.) for use with inflation devices, such propellants will not burn and thus, are of no use in accomplishing the objectives of this invention.
 
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