Propellant formulation and process

Details Propellant formulation and process Propellant formulation and process

1988-11-10

1995-02-14

Nelson, Peter A.

Ammunition and explosives

Powder form

Having embedded reinforcing or burning control means

102290, 149 37, 149 38, 149114, C06D 506, C06B 3300

Patent

active

053885180

ABSTRACT:
The present invention relates to metal filaments for use as fuel additives for rocket propellants, explosives, and other pyrotechnic devices. Preferred filaments are those such as zirconium, niobium and titanium (and alloys thereof) which have very high heat of combustion.

REFERENCES:
patent: 3784419 (1974-01-01), Baumann et al.
patent: 4001057 (1977-01-01), Baldwin et al.
patent: 4380482 (1983-04-01), Sandell et al.
patent: 4424086 (1984-01-01), Christopher
patent: 4530728 (1985-07-01), Sayles
patent: 4756251 (1988-07-01), Hightower, Jr. et al.
patent: 4764229 (1988-08-01), Miekka et al.

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