Combustion inhibited rocket propellants

Explosive and thermic compositions or charges – Structure or arrangement of component or product – Coated component

Patent

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Details

149 11, 102103, C06B 4528

Patent

active

040921867

ABSTRACT:
Solid propellant charge bonded directly to combustion inhibition material comprising elastomeric or polymeric material containing a compatible particulate filler material constituting at least 50wt.% of the combustion inhibition material.

REFERENCES:
patent: 3954701 (1976-05-01), Schaffling

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