> If I had a heavy landing I would want
> that battery mass to be within the cart-wheeling wing some 50 metres in
> front of me, not crushing my spine into the instrument panel)- perhaps they
> could put it on a sliding beam?


I don't suppose there is much difference having 50 kgs of batteries or
50 kgs of solo motor (or Wankel for that matter) up your date. (50 kgs
of feathers would be different). Mostly however, SLG motors don't
enter the cockpit unless absolutely necessary, and by then the pilot
has probably left the building, so to speak. Via the NOAH ejektion
seat.

Perhaps the most persuasive argument is the fact that the cells would
be in one block and easy to change when the technology changes, unlike
batteries stuffed into wings. You can guarantee this happening by the
time the aircraft is in the air. Certainly by the time it has landed.

You probably only need to monitor the health of individual cells if
they are likely to explode like LiPolys. If the cells are
self-balancing like most rechargables, then this should not be
necessary.

There's a 4.5 kgs motor commonly available for UAVs which produces 13
KVA. An alternative and interesting solution is to have a group of
less powerful motors arranged around a large ring gear which gives
good redundancy. Most of the motors we see are hobby ones or similar.
If you go to the specialised suppliers, most of whom are in Germany,
you can get much greater power densities.

DMcD
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