High fuel regression hybrid rocket motor

Power plants – Reaction motor – Solid and fluid propellant

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60258, F02K 972

Patent

active

060148578

ABSTRACT:
A hybrid rocket motor having a multitude of radially inward directed miniature hybrid secondary combustion chambers within a single solid fuel block being oxidizer-fed by a single centrally positioned distributor and a system of radially outward-directed feed tubes. The feed tubes are sealed at their distant ends and have multiple orifices opening into the secondary combustion chambers to resemble a multitude of secondary conventional-injection hybrid motors within a single main hybrid motor.

REFERENCES:
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patent: 3177657 (1965-04-01), Strauss et al.
patent: 3203174 (1965-08-01), Sutherland
patent: 3315472 (1967-04-01), Moutet et al.
patent: 3434287 (1969-03-01), Caveny
patent: 3457727 (1969-07-01), Munger
patent: 3789610 (1974-02-01), Stone
patent: 4442666 (1984-04-01), Vetter

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