NASA NTRS · 19700005158
Development of high temperature materials for solid propellant rocket nozzle applications Quarterly progress report, 1 Jul. - 30 Sep. 1969
Abstract
Refractory metal and graphite composite research for solid propellant rocket nozzle applications
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Lineback, L. D., Manning, C. R., Jr.. 1969-10-01. Development of high temperature materials for solid propellant rocket nozzle applications Quarterly progress report, 1 Jul. - 30 Sep. 1969. https://ntrs.nasa.gov/citations/19700005158
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