Multi-layer high energy propellants

US5690868A · kind A · utility

Assignee

• The United States of America as represented by the Secretary of the Army · US

Inventors

• Bernard Strauss · Rockaway, US
• Thelma G. Manning · Montville, US
• Joseph P. Prezelski · Budd Lake, US
• Sam Moy · Parsippany, US

Key dates

• Filing date: Nov 7, 1996
• Grant date: Nov 25, 1997
• Expiry date: Nov 7, 2016

Classification

• Technology area (CPC C): Chemistry; Metallurgy
• CPC primary: C06B45/12
• WIPO field: Basic materials chemistry
• WIPO sector: Chemistry

Abstract

A multi-layer propellant and a method for making the same is provided, in ich the propellant has at least one slow burning formulation and at least one fast burning formulation, such that the ratio of these burning rates is at least 2:1. The propellant produces an impetus of at least 1300 Joules/gm. The preferred binder is a high energy oxetane thermoplastic elastomer. The preferred slow burning formulation employs RDX, while the preferred fast burning formulation employs CL-20. The two formulations are formed separately, such as in layers that are then fused, using the bonding strength of the binder. The shape may be any shape that is useful in munitions and may include one or many layers of each burning rate. Preferred shapes include a multi-layered propellant with one slow burning formulation on top and a bottom layer of the fast burning formulation. The layers may be formed from ribbons, discs, cones, truncated cones and partial spheres. The amount of binder in each formulation should be sufficient to provide a uniformly dispersed oxidizer throughout the layer. Preferred amounts of binder range from about five percent to about thirty percent by weight, based on the total weight…