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Fluidic pressure regulatorsThree 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.
Document ID
19720000162
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mangion, C.
(TRW Systems Group)
Miller, W.
(TRW Systems Group)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Mechanics
Report/Patent Number
ARC-10474
Report Number: ARC-10474
Accession Number
72B10162
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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