Electric power allows you to have lots of small fans, a few of which can fail without disaster.
Also, throttling turbines up and down fast enough to stabilize an aircraft doesn't seem to work well.
Electric power allows you to have lots of small fans, a few of which can fail without disaster.
Also, throttling turbines up and down fast enough to stabilize an aircraft doesn't seem to work well.
There are plenty of ways to stabilize an aircraft without relying on pure engine thrust, and turbofan aircraft have some advantages here.
The distributed electric propulsion systems do have awesome redundancy, but they have significant losses in efficiency compared to fewer, larger props, which really isn't what you want in an aircraft with severe energy density limitations. I'm curious to see what the production Lillium's payload, range, and power margin end up being.