For example, an aircraft could "start" at 50% battery state of charge, then charge to 95% over the course of the day, then come back 24 hours later at 51%, and that would be valid. There are other ways around this, but this is what I came up with at the time.
This is similar to why the starting altitude is allowed to float. The gravitational potential energy of the aircraft can be used as another "battery", but the aircraft is only a valid solution if it's not losing altitude over the course of 24 hours.
Various metals can be used. Iron is cheap, whilst aluminium-air cells actually offer some of the best performance in kWh/kg of available materials, exceeding that of LiON cells.
https://en.wikipedia.org/wiki/Metal%E2%80%93air_electrochemi...
edit: remember the context. This is about an abstract optimization to find the minimum viable aircraft.
see: https://physics.stackexchange.com/questions/34421/does-the-m...
A fully charged battery would necessarily have more mass than a fully depleted battery, but the difference should be so tiny as to be immeasurable. Or am I wrong? We're essentially talking about the sum weight of a bunch of electrons, which are extremely light. There's no other exchange of matter going on when charging/discharging a battery, just the creation/destruction of chemical bonds, and associated movement of electrons.
However it has less potential energy. And therefore you change mass by the mass associated with that potential energy.
Is it feasible to operate these at lower altitudes?
e.g. can we have solar/air drones posted every 100 miles of interstate highway?!
What's the usefulness of this or was it just a random example?
Nobody likes photo radar.