A fixed-wing drone comprising: a main body; a left main wing and a right main wing; a left forewing and a right forewing, which are shorter than the left main wing and the right main wing; a left linear support, which physically connects.the left forewing to the left main wing and which is fixed near a left terminal end of the left forewing; a rear terminal end of the left linear support extends rearward beyond a rear edge of the left main wing; a right linear support, which physically connects the right forewing to the right main wing and which is fixed near a right terminal end of the right forewing; a rear terminal end of the right linear support extends rearward beyond a rear edge of the right main wing; a left linear alignment of propellers having a first propeller, a second propeller, and a third propeller; a right linear alignment of propellers having a fourth propeller, a fifth propeller, and a sixth propeller; wherein the left linear alignment is parallel to the right linear alignment, the first propeller, the second propeller, and the third propeller are directly disposed linearly in a straight line on the left linear support, wherein the straight line is parallel to a longitudinal axis of the main body, the first propeller is disposed at the front terminal end of the left linear support, the third propeller is disposed at the rear terminal end of the left linear support, the fourth propeller is disposed at the front terminal end of the right linear support, and the sixth propeller is disposed at the rear terminal end of the right linear support, characterized in that, the left linear support is fixed at a front terminal end near the left terminal end of the left forewing, the right linear support is fixed at a front terminal end near the right terminal end of the right forewing, and the first propeller and the second propeller are disposed on opposing sides of the left linear support. a main body; a left main wing and a right main wing; a left forewing and a right forewing, which are shorter than the left main wing and the right main wing; a left linear support, which physically connects.the left forewing to the left main wing and which is fixed near a left terminal end of the left forewing; a rear terminal end of the left linear support extends rearward beyond a rear edge of the left main wing; a right linear support, which physically connects the right forewing to the right main wing and which is fixed near a right terminal end of the right forewing; a rear terminal end of the right linear support extends rearward beyond a rear edge of the right main wing; a left linear alignment of propellers having a first propeller, a second propeller, and a third propeller; a right linear alignment of propellers having a fourth propeller, a fifth propeller, and a sixth propeller; wherein the left linear alignment is parallel to the right linear alignment, the first propeller, the second propeller, and the third propeller are directly disposed linearly in a straight line on the left linear support, wherein the straight line is parallel to a longitudinal axis of the main body, the first propeller is disposed at the front terminal end of the left linear support, the third propeller is disposed at the rear terminal end of the left linear support, the fourth propeller is disposed at the front terminal end of the right linear support, and the sixth propeller is disposed at the rear terminal end of the right linear support, characterized in that, the left linear support is fixed at a front terminal end near the left terminal end of the left forewing, the right linear support is fixed at a front terminal end near the right terminal end of the right forewing, and the first propeller and the second propeller are disposed on opposing sides of the left linear support.