1967-02-01

An Approach to Simpler Control Requirements 670138

A control system requirement is defined for an advanced direct lift engine designed for a typical Mach 2 fighter aircraft. The characteristics of the control system (performance, weight, reliability and maintainability, cost) are shown to be predominantly a function of the degree of simplicity of the control system requirements and somewhat less a result of the mechanization employed to meet those requirements.

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