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This paper identifies critical and relevant variable/adaptive cycle turbine engine and propulsion subsystem technologies for future next generation aviation systems. A comprehensive evaluation of key technology drivers associated with the development and demonstration of advanced Adaptive Power and Thermal Management System (APTMS) technologies applicable to next generation platforms is addressed. Specifically, the paper explores energy optimization through dynamic mission based simulations of an advanced hybrid air cycle / vapor cycle APTMS architecture combining multiple traditionally federated subsystem functions including auxiliary power, environmental control, emergency power, and engine start.

Pairing of a high-speed, high-temperature superconducting, homopolar inductor alternator (HTSHIA) with a gas turbine engine as prime mover results in a power dense generator-set well suited to applications requiring large step load accepts and rejects. Though the HTSHIA's low synchronous reactance allows it to respond to large step loads, typical gas turbine engines require seconds to ramp from idle to full power. A mismatch between load and turbine power during a step transient will result in generator speed droop. If the speed droops too severely either the generator or gas turbine engine may no longer be able to maintain rated power. This paper presents a generator set and control approach which exploits the HTSHIA's flywheel properties (high speed and relatively high rotor inertia) to power large, repeated step loads.