This is not about financial cost, it is about weight and complexity. It would be less costly and more efficient to separate water into hydrogen and oxygen (using solar power if you like), then use them to power a rocket engine.
1) Aircraft cost is proportional to empty weight.
2) Range is proportional to total stored energy / drag and drag is proportional to weight. If you have low specific energy, you cannot go far.
And it's true that airliners take off with more weight than they are speced to land with. They have to dump fuel if landing before burning it off.