Rocket motor

Power plants – Reaction motor – Solid propellant

Patent

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Details

102531, 102284, F02K 914, F02K 938

Patent

active

043110053

ABSTRACT:
An improved rocket motor using a solid propellant is shown to include a perforate shield disposed between a combustion chamber and a nozzle to prevent any portion of the solid propellant from entering the nozzle during operation.

REFERENCES:
patent: 694295 (1902-02-01), Maxim
patent: 952538 (1910-03-01), Luciani
patent: 3898934 (1975-08-01), Mercier
patent: 3991683 (1976-11-01), Rentzsch et al.

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