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Axial force is a key parameter for many aeroscience R&D applications. Axial force is the dominant component used to measure aircraft drag (for fuel efficiency purposes) and provides important control information (such as vehicle deceleration rate). Integration of Axial force measurement into this design enables a direct measure of the drag force, while simultaneously providing a fluid flow path for powered simulation in wind tunnel testing. Current state-of-the art alternatives (i.e., flow-through balances without axial force) either require investigators to infer the drag force by integrating pressure taps on the test article (which further increases axial force measurement uncertainty) or run a redundant, second wind tunnel entry with a standard six-component balance without the flow-through capability (which is not desirable because they are expensive, time consuming, and impede efficiency). While NASA’s flow-through transducer technology could be manufactured using conventional fabrication methods, additive manufacturing is expected to be preferred as it enables relatively simple incorporation of the flow-through axial element into the design without increasing manufacturing complexity or costs.