NASA NTRS · 19730024028
Omni-axis secondary injection thrust vector control system
Abstract
The 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.
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Kirkley, D. J.. 1973-07-18. Omni-axis secondary injection thrust vector control system. https://ntrs.nasa.gov/citations/19730024028
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