NASA NTRS · 19660003585
Refractory thrust chambers for spacecraft engines Final report
Abstract
Structural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid propellant rocket engine thrust chambers and nozzles
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Campbell, J. G., Coulbert, C. D.. 1965-03-22. Refractory thrust chambers for spacecraft engines Final report. https://ntrs.nasa.gov/citations/19660003585
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