Alright, folks. Given the lackluster hearing, why dont we take an opportunity to rule out some things with the official government data on UAP cases?

Problem: What amount to energy is required for the following object to lift and function?

Size: 2-4 meters spherical Material: Metallic alloy (Zinc, Aluminum, Copper, Steel, Iron, Titanium, Nickel) Weight: Unknown, but with size and material estimates can be drawn for each alloy. Height: 10,000-50,000 ft (3048m-15240m) Speed: Maximum of Mach 2 (686 m/s) Composition: One model solid, one model hollow (weight decrease by 75%)

We cannot determine the propulsion, but we can determine the average Joules of energy required for lift and thrust. Once we have that, we can start to rule out fuel sources based on expected exhaust signatures.

Let's put this down on paper and throw it at Avi Loeb and team. While DoD is arguing over funds and pointing fingers at each other for alow progress, the community can get some actual work done.

Who's up for the task?