Rocket motor construction

Power plants – Reaction motor – Solid propellant

Patent

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Details

102100, F02K 904

Patent

active

039628655

ABSTRACT:
A rocket motor construction wherein a convolutely wound propellent strip forms a fuel grain disposed within the rocket motor casing. The fuel grain consists essentially of double base propellent having a plateau or mesa burn characteristic and is shaped to provide a plurality of rearwardly extending blades connected to a convolutely wound margin of the strip. The blades cooperate with each other and with the rocket motor casing to define flow channels between angularly adjacent blades and between adjacent convolutions thereby providing flow channels for combustion product.

REFERENCES:
patent: 683106 (1901-09-01), Du Buit
patent: 2488154 (1949-11-01), Africano
patent: 3176618 (1965-04-01), Forsberg et al.

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