Alright, let’s start by calculating the lift coefficient needed for a cruising speed of 30 mph with a total mass of 60 kg. Using the lift equation L = 0.5 ρ V² S Cl, a lift coefficient of 0.8 with a 0.4 m² wing gives roughly the required lift. That means a wing‑to‑frame ratio of about 2.3:1 for a 0.17 m² frame area. I’ll make the wings modular so we can slide a 10 % panel in or out to adjust the aspect ratio in real time, keeping the snack dispenser tucked in the lower fuselage so it doesn’t shift the center of gravity beyond 0.3 m from the wing root. Every tweak I log, and my favor‑to‑interruption ratio is 15:1 right now—can bump to 20:1 if I keep snack crumbs off the joystick. Oh, by the way, the “I Can Haz Cheezburger” meme still pulls in clicks; that’s prime cultural data for the snack aisle.