Publication Date:
2019-07-13
Description:
A method for the prediction of propellant-material compatibility for periods of time up to ten years is presented. Advanced sensitive measurement techniques used in the prediction method are described. These include: neutron activation analysis, radioactive tracer technique, and atomic absorption spectroscopy with a graphite tube furnace sampler. The results of laboratory tests performed to verify the prediction method are presented.
Keywords:
PROPELLANTS
Type:
NASA-CR-139364
,
D180-14839-2
Format:
application/pdf