No where does it mention proposed range. This is a big deal: with thirsty supersonic cruise, your fuel mass fraction will exponentially grow according to the Rocket Equation. Simply put, the more fuel you carry, the more fuel you must carry to bring that fuel along. Flying twice the distance will mean >>2x the fuel. LON-NYC might be attainable, but tran-pacific will certainly be difficult.
The rocket equation applies when you're continuously accelerating your fuel to ever higher speeds. The work in supersonic flight is fighting drag, which while many times larger that for subsonic does not have an appreciable weight dependency. Why would flying longer require more than proportionally additional fuel?
I know this is certainly true of subsonic flight. How much it affects supersonic flight it unknown to me.