Oxidizer package for propellant system for rockets

F - Mech Eng,Light,Heat,Weapons – 02 – K

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F02K 9/00 (2006.01)

Patent

CA 2322069

A package of oxidizer for a propellant system for a motor in which said oxidizer is separated from fuel grain, said package comprising oxidizing material and an ignition system therefor in a wrapping or sealing material. A hybrid rocket comprising oxidizing material and fuel grain, said oxidizing material being separated from the fuel grain and being in the form of a single package or plurality of packages of oxidizing material and an ignition system therefor, said packages generally conforming to the shape of the rocket. A grid of a pyrotechnical material. A propulsion system for a hybrid rocket comprising oxidizing material in a matrix, mesh, wool, foamed metal or wires of structural or pyrotechnical material.

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