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NASA NTRS · 19910015918

Temperature automation for a propellant mixer

Abstract

The analysis and installation of an automatic temperature controller on a propellant mixer is presented. Ultimately, the entire mixing process will come under automation, but since precise adherence to the temperature profile is very difficult to sustain manually, this was the first component to be automated. Automation is not only important for producing a uniform product, but it is necessary for envisioned space-based propellant production.

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BibTeXRIS

Vincent, T. L., Wilson, R. G.. 1990-01-01. Temperature automation for a propellant mixer. https://ntrs.nasa.gov/citations/19910015918

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