So, I think that high-altitude sparse-population daytime routes could be developed that would admit supersonic flight over much of North America.
Of course being a little no-name company won't help matters much here, but I expect that actual production of this would involve a partnership (or probably buyout) with one of the big name companies that have a lot of congressmen on their payroll.
There has also been a lot of research into minimizing Sonic Booms since the 70s. Military jets typically don't care, but passenger jets could definitely benefit.
It's a good way to kick everyone in a large region out of their zone. If this was a constant occurrence, work may quickly cease, or become greatly diminished.
And I do wish humans where mindful about the noise pollution the dump where 'nobody lives'. The noise emitted by shipping vessels is having a harming effect on sea life.
Concorde was really, really loud --- a lot of that was due to being a really old plane with old engines (aircraft have gotten way quieter since the 1970s), but even back then it was considered loud:
http://news.bbc.co.uk/2/hi/uk_news/3581192.stm
It was exempt from the usual noise regulations and on takeoff it'd set of car alarms in the airport carparks.
I still miss it, despite the noise. I'd hear the noise and look up, and there'd be this beautiful delta-wing shape slipping through the clouds...
...yeah, yeah, I know, being dull is an accomplishment in itself, and the duller aircraft are the better they are, and the one thing that every passenger pilot in the world wants is a thoroughly uninteresting flight. But, dammit, they're still so dull.
I miss Concorde.
Boom's Kenrick Waithe worked on that same project when he was at Gulfstream and when he was at NASA.
[1] - https://en.wikipedia.org/wiki/Oklahoma_City_sonic_boom_tests
This whole "engineering vs physics" question reminds me of the misunderstandings people have of modern radio technology. Yes, in the 1920s they had to divide the spectrum into exclusive-use bands so that any particular use could transmit and receive clearly, but that was a limitation of engineering, not of physics. In the 2010s that is not a limitation we face, in general. Likewise, I expect that with modern materials and engineering software, progress can be made on the sonic boom issue.
If - via engineering, physics, magic or whatever - sonic booms can be minimized to the point of being indistinguishable from general background noise (or even only as intrusive as current subsonic airliners), I could be convinced that an SST project has a bright future. Until then, I don't think that they will - your first post mentioned that "the whole house shaking" didn't really seem to be hardship when it happened during the day; I'm merely commenting that there are some studies that indicate society as a whole isn't so accepting.
I think any design that literally goes "boom" over land, even a little, isn't going to work. It's too much of an open legal target.
The design really does need to be damn near silent, or at least closer to a mild and unobjectionable "whomp", to have any hope of commercial success.
Cruising above 60000 ft the boom from a larger aircraft might be noticed but not be objectionably loud.
Transonic (approximately Mach 0.80 - 1.2) flight uses significantly more fuel than subsonic flight does. Business jets like the Gulfstream G550 burn more fuel at M0.9 than regional Boeing 717(MD-95) at M0.75 with 4 times more passengers.
The F-22 Raptor can supercruise at M1.6, with half the range compared to cruise at M0.85 similar to other fighters.
If Boom can optimize an aircraft for supersonic transport it would still be expensive to operate. For comparison, no US operator has all business class scheduled flights from LA-NY, and British Airways flies their all business class NY-London flights in an VIP A320 series jet that cruises at M0.7 which is slower than most airliners on the route.
There has never been a supersonic passenger aircraft built with modern turbofan engines.
Test pilots have reported that a Gulfstream G550 airframe can handle supersonic flight, and the BR710 turbofan engines can handle it. The limit is the engine intake design.
With an optimized intake, its entirely possible the fuel consumption at M2.2 would be comparable to ~M0.98
that is one of the major issues here. Modern turbofans on large passenger planes like 787, 380, etc... are that efficient in major part because of high by-pass ratio. Which is not really an option for 2Mach+ speed.
As somebody mentioned, more comfortable 0.85Mach flight would be preferable in many situations to uncomfortable and very expensive 2Mach. If i were starting something like this i'd go straight for suborbital SFO to Singapore in under couple hours. Technology-level wise not that different, money is no issue in that segment (Branson's $200K is not that far from super-premium-business class for your priceless CEO) and there is always large money-no-issue fallback customer - military.
[edit] As someone who flies LA/DC fairly regularly I do have to mention my favorite record of the SR-71 doing that flight in under 65 minutes.