SHOCK COMPRESSION BASED SUPERSONIC COMBUSTOR
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United States of America Patent
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Issued Date -
Jan 11, 2018
app pub date -
Jun 14, 2016
filing date -
Jun 14, 2016
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Abstract
A supersonic combustor containing an injector module, a combustor core and an outer shell. The injector module houses both fuel and oxidizer nozzles. The combustor core contains grooves within which the combustion process takes place. The outer shell holds both the injector module and the combustor core and allows for other cooling, mounting and structural mechanisms required for operation.
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