This report contains the result of a study contract from CAE to design and lay out a fuel control which would operate a rotor tip mounted engine (CAE Model 357-1) in a 235g field.nBased on preliminary tests and analytical design studies, the fuel control system recommended is a combined hydromechanical and electronic control system which includes an engine-driven fuel pump. Figure 7 is a schematic of the control system. Studies indicate that the proposed design can be developed so that production components can be assembled without requiring special whirl-rig-component balancing tests.
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