High energy propellant formulation

Details High energy propellant formulation High energy propellant formulation

1990-12-14

1994-08-02

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

C06B 4510

Patent

active

H00013412

ABSTRACT:
A high energy rocket propellant can be formed wherein the propellant binder has a cellulose acetate butyrate: polyethylene glycol ratio of about 0.01 to 0.03 on a weight basis.

REFERENCES:
patent: 4216039 (1980-08-01), Pierce
patent: 4234364 (1980-11-01), Robinson
patent: 4379903 (1983-04-01), Reed et al.
patent: 4670068 (1987-06-01), Chi
patent: 4804424 (1989-02-01), Hinshaw
patent: 4925504 (1990-05-01), Sayles

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