NASA NTRS · 19720000162
Fluidic pressure regulators
Abstract
Three basic areas for possible application of fluidic control to rocket engine subsystems were identified and six subsystem configurations were analyzed for study. Results provide indication of tradeoffs involved between conventional and fluidic regulators and should be of interest to control and applications engineers who need to make similar analyses.
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Mangion, C., Miller, W.. 1972-01-01. Fluidic pressure regulators. https://ntrs.nasa.gov/citations/19720000162
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