Solid propellant gas generating device

Power plants – Reaction motor – Solid propellant

Patent

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Details

102103, F02K 904

Patent

active

041201531

ABSTRACT:
1. In combination with a vessel forming a rocket motor combustion chamber, a rubber-base liner firmly adhering to the interior chamber wall, said rubber-base liner containing between about 2.5 and 30 percent by weight of an inorganic metal salt selected from the group consisting of zinc chromate, barium chromate, zinc phosphate, lead phosphate, potassium phosphate, and mixtures thereof, and a propellant charge substantially filling the lined portion of the chamber, said propellant charge firmly adhering to said liner.

REFERENCES:
patent: 2479470 (1949-08-01), Carr
patent: 2563265 (1951-08-01), Parsons
patent: 3012508 (1961-12-01), Stanley
patent: 3032437 (1962-05-01), Pitchford
patent: 3046829 (1962-07-01), Roemer
patent: 3144829 (1964-08-01), Fox

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