But AAI believed Jay Carter's reinterpretation of the autogyro offered the promise of an affordable VTOL capability for unmanned aircraft, without the weight, complexity and maintenance burden of a conventional helicopter's powered rotor.
Initially, AAI's focus for SR/C was on adding an unpowered rotor to the RQ-7 Shadow to produce a tactical UAV that, by virtue of VTOL capability, would be independent of both rail launchers and runways. It has also studied a larger cargo UAV using SR/C and uses the technology in its Transformer "flying Humvee" design for DARPA.
Now the company has unveiled the Shadow Knight, its contender for the US Navy's Medium-Range Maritime Unmanned Aerial System (MRMUAS) requirement for a shipboard VTOL UAS significantly more capable than the MQ-8 Fire Scout.

Concept: AAI, via Mike Hirschberg
Shadow Knight uses SR/C technology, but with a twist. Where Carter's design can take off and land vertically by first spinning up the high-inertia rotor, it can't hover. Recognizing that getting on and off a ship will require the ability to hover, AAI plans to add the capability to power the rotor.
That would seem to negate the principal benefit of SR/C - that it's unpowered rotor is simpler and easier to maintain than a conventional helicopter dynamic system. But AAI argues that the clutch and transmission needed to drive the rotor during take-off and landing would have a much lower duty cycle, and maintenance burden, than a helicopter drive system.
In forward flight, Shadow Knight would still fly like a compound autogyro. Props would provide forward thrust, the now-autorotating rotor would be slowed to minimize drag, and lift would transfer to the aerodynamically efficient long-span wing. The result, AAI believes, would be greater speed and endurance than a conventional helicopter.
AAI's data sheet for the Shadow Knight says it would meet the MRMUAS requirement to provide continuous surveillance at 300nm from the ship while carrying an 880lb ISR/strike payload. Dash speed would be up to 230kt and an additional 33 cu ft of payload space would provide a cargo resupply capability.
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