The problem is, at supersonic speeds, air starts to act more like water.
Aluminum is cheap; but making an “SS-anything” out of aluminum would require the parts to be so massive that it would take REALLY prohibitively expensive power to even make it fly at all.
So, aluminum is replaced with titanium and other exotics.
So the SST (go find pictures) was reduced to a tiny needle that landed so hot that the cockpit had to hinge downward for the pilots to see.
Every flight was subsidized by the Anglo-French consortium which built them.
Over land, it could not do its supersonic thing - every country it wanted to go to had rules about sonic booms.
I once worked with an ultimate Yuppie - he had money enough and ego enough to buy a ticket. Unfortunately, it was not trans-oceanic, so the airspeed display in the cabin never went over .9 mach.
The Boeing entrant was named the 7007 (note the zeroes), if you want to search.
It was my suspicion that, because of the “civilized hostility” between the British and the French (France blocked the UK’s into the EEC (forerunner of the EU), for instance), it became a matter of one-upmanship as the realities of the limits and costs became obvious - neither was going to suggest the obvious - let’s not do this. Ever see two kids in a staring contest?
And the BD10J was a two-seater. All the billionaire who would drop a bit over a million to have one built would need to do was find a pilot qualified to fly it.
Pilots: aside from “Complex Aircraft”, what credentials would the FAA require to operate a 2 seater at mach 1.1?
It isn’t over 12,500 pounds, but I suspect some kind of endorsement would be required.
What did the Russians want to see before allowing the rider to take the stick in the MiG-29, for instance?