Publication Date:
2019-06-27
Description:
A report on the effects of fuel vortex film cooling on high temperature coating durability is presented. The program evaluated candidate high temperature oxidation resistant reaction control system engine thrust chamber material. As a result of the evaluation, the current and future programs may be optimized from the materials standpoint. Engine firing data for the evaluation of one material system is generated. The subjects considered are: (1) screening of materials, (2) thrust chamber fabrication, (3) engine testing, and (4) analysis of the data.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
NASA-CR-141450
,
REPT-8701-910045
Format:
application/pdf