Propellant formulations based on dinitramide salts and energetic

Details Propellant formulations based on dinitramide salts and energetic Propellant formulations based on dinitramide salts and energetic

1993-04-21

1996-03-12

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

149 194, C06B 4510

Patent

active

054983037

ABSTRACT:
Composite propellant formulations are disclosed having a dinitramide salt oxidizer, such as ammonium dinitramide, an energetic binder, such as poly(glycidyl nitrate), a reactive metal, such as aluminum, and other typical propellant ingredients such as curatives and stabilizers. The disclosed propellant formulations are able to combust aluminum efficiently, possess high burn rates, and produce little or no HCl exhaust gases.

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