Combustion chamber for a ramjet and booster rocket

Details Combustion chamber for a ramjet and booster rocket Combustion chamber for a ramjet and booster rocket

1978-09-06

1980-05-20

Garrett, Robert E.

Power plants

Reaction motor

Motive fluid from diverse generators alternatively ejected...

60250, F02K 904

Patent

active

042032849

ABSTRACT:
The invention relates to a combustion chamber of a ramjet and booster rocket, which comprises an inner envelope provided with upstream lateral ports for the inlet of air and a downstream nozzle for ejecting the combustion gases, to allow functioning of the rocket at cruising speed; an outer envelope, concentric to the inner envelope and closed, with the exclusion of a single rear port for the ejection of the gases, to allow functioning of the rocket at launching speed; and separating means for separating from the combustion chamber at least a part of the outer envelope, at the end of the launching phase, in order to ensure the clearance of the upstream lateral ports of the inner envelope.

REFERENCES:
patent: 3357187 (1967-12-01), Whitlock

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