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Omni-axis secondary injection thrust vector control systemThe concept, development, design study and preliminary analysis and layout of the required digital logic scheme to be used for injection valve control are presented. An application and optimization study of an Omni-Axis Secondary Injection Control System applicable to the proposed Space Shuttle Pressure Fed Engine is reported. Technical definition and analysis control procedures and test routines, as well as a supporting set of drawing sketches and reference manual, are enclosed.
Document ID
19730024028
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kirkley, D. J.
(E-Systems, Inc. Salt Lake City, UT, United States)
Date Acquired
September 2, 2013
Publication Date
July 18, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-124428
Report Number: NASA-CR-124428
Accession Number
73N32761
Funding Number(s)
CONTRACT_GRANT: NAS8-28887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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