Propellant formulation and process

Details Propellant formulation and process Propellant formulation and process

1989-10-23

1995-04-11

Nelson, Peter A.

Ammunition and explosives

Powder form

Having embedded reinforcing or burning control means

149 37, 149 38, 149114, C06B 4500

Patent

active

054048133

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: 4764422 (1988-08-01), Miekka et al.

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