4 ms·
Yeah, I worry that a lot of the use cases are in the most complicated and dangerous flight environments (mountains, big cities), even before you consider things
by scarier 6y ago
Yeah, I worry that a lot of the use cases are in the most complicated and dangerous flight environments (mountains, big cities), even before you consider things like weather, airspace management, power margin at altitude...
>Also, I find the lack of a vertical stabilizer this plane to be an odd choice.
Not to mention any form of traditional aerodynamic control surface: "With 36 single-stage electric motors providing near-instantaneous thrust in almost any direction, control surfaces, such as rudders, ailerons or a tail, aren't required."
They've really doubled down on their VTOL shindig. Seems like a pretty big gamble making an aircraft that's entirely dependent on its propulsion system for basic aerodynamic stability and control (I'm also curious if the wings would make noticeably less lift in a glide). "Intrinsically simple design," huh?
- steffan 6y agoGiven enough redundancy in the powertrain and power, I think it's probably going to be more reliable mechanically than the average piston-engined light aircraft. Where I would really worry, of course, is the software driving all of that. It's very likely it will need some sophisticated control systems and may not even be inherently stable aerodynamically.