Power plants – Reaction motor – Solid and fluid propellant
Patent
1975-02-13
1977-01-04
Freeh, William L.
Power plants
Reaction motor
Solid and fluid propellant
60258, 60 3974A, 239417, 239584, F02K 906, B05B 712
Patent
active
040006131
ABSTRACT:
A dual orifice injector assembly for use in a hybrid rocket motor having a oost and sustain mode and capable of controlling liquid flow rate for the two different modes of operation comprising an inlet manifold to distribute the fluid through a sustain injector and boost injector, actuating means for axially moving the sustain injector into a position to close off the boost injector for the sustain mode of operation and a flow deflector to cause the fluid to be dispersed in a fan like pattern at an angle 180.degree. to the axis of the manifold housing.
REFERENCES:
patent: 2085800 (1937-07-01), Goddard
patent: 2214757 (1940-09-01), Alden
patent: 2411667 (1946-11-01), Mowrey
patent: 2720845 (1955-10-01), Whitlock
patent: 3064903 (1962-11-01), Butler
patent: 3216693 (1965-11-01), Hook
patent: 3431733 (1969-03-01), Hamrick
patent: 3515353 (1970-06-01), Young et al.
patent: 3742701 (1973-07-01), Feemster et al.
Fukumoto Akiharu
La Force Phil D.
Freeh William L.
Garrett Robert E.
Miller Roy
Sciascia R. S.
The United States of America as represented by the Secretary of
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