A further general consideration necessary to proper ramjet-engine development concerns the role which the fuel system plays in such development. While steady progress is being
made toward making the design of combustors and diffusers an
exact science there remains a certain amount of art in the design of each of these engine components. Further, the testing
of these engine components is a costly operation. In order to
proceed with airframe design, it is necessary to specify the
diffuser and, to a lesser extent, the combustor at an early
stage in the engine program. The fuel system must therefore
adjust to the detailed performance of these components, as later determined, in order to secure optimum engine performance.
Sufficient flexibility must be provided in the functional relation between fuel flow and speed and atmospheric conditions of
flight to permit adjustment at a late stage in engine development .
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