Propellant formulation and process containing bi-metallic metal

Explosive and thermic compositions or charges – Containing free metal or metal hydride with hydrocarbon or...

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Details

149 40, 1491082, 149114, C06B 2700, C06B 3312, D03D 2300

Patent

active

053485971

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: 4764229 (1988-08-01), Miekka et al.
patent: 5212343 (1993-05-01), Brupbacher et al.

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