Rocket thrust chamber

Power plants – Reaction motor – Including heat exchange means

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Details

60266, 60 3932, F02K 964

Patent

active

058327193

ABSTRACT:
A thrust chamber for an expander cycle rocket engine having a predetermined quantity of tubes concentric about an axis and radially inward of a structural jacket, each tube having first and second substantially planar sidewalls which diverge at an angle such that immediately adjacent tubes are in spaced relation to each other at the radially inward portion of each tube.

REFERENCES:
patent: 2844939 (1958-07-01), Schultz
patent: 2958183 (1960-11-01), Singlemann
patent: 3049870 (1962-08-01), Chamberlain
patent: 3066702 (1962-12-01), Tumavicus
patent: 3190070 (1965-06-01), Neu, Jr.
patent: 3208132 (1965-09-01), Escher
patent: 3595025 (1971-07-01), Stockel et al.
patent: 3692637 (1972-09-01), Dederra et al.
patent: 3798902 (1974-03-01), Butter
patent: 3835644 (1974-09-01), Butter et al.
patent: 5233755 (1993-08-01), Vandendriessche

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