COMBUSTION CHAMBER FOR LIQUID LOW-THRUST ROCKET ENGINE Russian patent published in 1995 - IPC

Abstract RU 2041375 C1

FIELD: space engineering. SUBSTANCE: chamber has housing 14 and mixing head 1 with two-component centrifugal nozzle 8 wherein outer 7 and inner 11 space are connected with collectors 4 and 5 of fuel components respectively. The chamber is also provided with a set of jet nozzles, the inlet of each of the nozzle being connected with manifold 4. The projection of the axis of each jet nozzle on the plane of the head is perpendicular to the radius at which its outlet is arranged. EFFECT: improved design. 3 dwg

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RU 2 041 375 C1

Authors

Andreev Ju.Z.

Ermolovich E.I.

Larin E.G.

Dates

1995-08-09—Published

1990-02-28—Filed