NASA NTRS · 19660021049
Localized overheating in Aerobee regeneratively cooled thrust chambers
Abstract
Overheating in convergent section of Aerobee rocket combustion chamber nozzle due to nozzle design and regenerative cooling system
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Bushnell, P. S., Jr., Busse, J. R.. 1966-03-01. Localized overheating in Aerobee regeneratively cooled thrust chambers. https://ntrs.nasa.gov/citations/19660021049
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