Available Technology

Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing

A supersonic combustion apparatus and method of using the same including a side wall cavity having an enhanced mixing system with ground-based oxygen injection for hypersonic material and engine testing.
Inventors: 

Timothy P. Parr, Ken Yu, Jaul Warren, Kenneth J. Wilson

Patent Number: 
US6948306
Patent Issue Date: 
October 27, 2005
Lab Representatives
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