No.Still, wouldn't an autogyro require a takeoff and landing roll of some sort?
See aboveGranted, it will be far sorter than that of a comparable fixed-wing aircraft, but on the cramped flight deck of an LHA/LHD, this could still be a constraint.
Plus, once you get the autogyro up to full combat loads (gas, cargo, and fully-armed troops, plus any additional mission equipment (door guns, etc.), the takeoff roll could be even longer.
An autogyro is not a helicopter. It requires forward motion for flight. So you can take off vertically by "spinning up" the rotor, but you cannot land the same way unless you power the rotor again as in your example below (the rotodyne). It is however simple to make, robust and simple to fly and land.Also, would an autogryo be able to sling-carry loads? I'm not an expert on air assault, but it seems to me like an aircraft that cannot truly hover might have some difficulty in picking up and dropping sling-carried loads.
The guy is doing an academic study, to (I would presume) get him to study the problems associated with Naval Air Operations. Everything to do with an aircraft carrier of any sort is a compromise, so it is a great way for students to learn to think "outside-the-box". It is not a full blown mission requirement,Perhaps a compromise might be achievable? Something like the Fairey Rotodyne?
One a related note: (Marines Plan Pick for Cargo UAS Demo)
:type
In reality, the most cost effective solution is to build a bigger aircraft carrier and a tilt rotor that can actually lift a useful load. The whole reason the V-22 blew out in cost were ridiculous "deck footprint" and replacement of the CH46 constraints. Bigger aircraft carriers mean less aerial compromises, that means uber savings in aerial platform development, while giving a couple of blue collar workers some more employment.
circa 22 Billion USD later? Beula? Anyone? Even a total conversion of the WASP class fleet to angled decks would have cost less.
It all comes down to the color of money and that is largely why you get these program inefficiencies.
cheers
w