Rapid Analysis and Manufacturing Propulsion Technology (RAMPT)

Fikes, John C

关键词: ASSEMBLIES;    COMBUSTION CHAMBERS;    COST REDUCTION;    DESIGN OPTIMIZATION;    FABRICATION;    REGENERATIVE COOLING;    THRUST CHAMBERS;   

RP-ID  :  MSFC-E-DAA-TN66349

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The RAMPT project is maturing novel design and manufacturing technologies to increase scale, significantly reduce cost, and improve performance for regeneratively-cooled thrust chamber assemblies, specifically the combustion chamber and nozzle for government and industry programs.