Combustor of high pressure burner for rocket engine and method of fabrication thereof

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United States of America Patent

PATENT NO 4909032
SERIAL NO

07337551

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Abstract

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An inner tube tube an outer surface of which is machined to define regerative coolant grooves for flowing a coolant to cool a combustor is split at a throat into upper and lower portions which in turn are fitted into an outer tube fabricated as a unitary structure. The upper and lower inner tube portions and the inner and outer tubes are integrally joined together.

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Patent Owner(s)

Patent OwnerAddress
ASTRONAUTICAL SCIENCEBOTH OF

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Higashino, Kazuyuki Sayama, JP 6 32
Horiuchi, Ryo Urayasu, JP 2 12
Saito, Satoshi Yokohama, JP 210 2550
Suzuki, Koichi Tokorozawa, JP 389 3939

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