NASA NTRS · 19790012952
Method of making a rocket nozzle
Abstract
A method is described for forming the interior of a nozzle having uneven walls so that a throat of smooth converging and diverging sides is provided for passing flow. A metallic insert material is placed within the flow passageway adjacent to the area where the sharper throat constriction is to be formed, so that the material will flow through the inlet into the throat space when liquefied.
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Campbell, D. H.. 1969-12-23. Method of making a rocket nozzle. https://ntrs.nasa.gov/citations/19790012952
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