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The pintle injector is one of the promising technique for variable-thrust rocket. We present a research aimed at the influences of axial liquid film instability on the spray characteristics of the pintle injector in the present study, as well as a modification scheme for the pintle post.

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This page is a summary of: Effects of Liquid Film Instability on Spray Features of Liquid–Liquid Pintle Injectors, AIAA Journal, November 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064017.
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