Rocket chamber heat exchanger

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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Details

C060S266000, C165S154000

Reexamination Certificate

active

07370469

ABSTRACT:
A rocket engine chamber has a back structure and a heat exchanger structure located radially inwardly of the back structure. The heat exchanger structure has a plurality of integrally formed cooling passageways with adjacent ones of the passageways having a common sidewall structure. Each passageway has a top section which forms the wall that contacts the hot gases. The top section is formed by a wall structure having an inner and outer surface formed by an arc of a circle and a substantially constant wall thickness.

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patent: 2003/0066636 (2003-04-01), Kawakubo et al.
NASA Contractor Report 187207, Thrust Chamber Material Technology Program, J.S. Andrus et al., Mar. 1989.

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