Some of the German concept studies a few years ago were looking for enough combat radius on internal fuel to be able to fly long CAP missions on NATO’s borders while operating from German bases, crossing all of Poland to reach the Baltics etc. I.e. 1hr CAP @ 550nm.
All that on internal fuel, with no drop tanks or air to air refueling, and a large payload (6 Meteors with no folding fins + 2 IRIS-T). Oh also with the ability to accelerate to Mach 2.0, loiter at 50,000ft, and excellent maneuverability. Basically that means a big airframe, a giant wing, and huge engines.
However what’s not clear is whether these were just thought exercises to see what could work, or hard requirements. Probably a mix of the 2.
Dassault’s philosophy would probably be to aim for a much lighter, less draggy airframe, maybe have it loiter a little lower (45,000ft), fly a little slower (Mach 1.8), and carry fewer Meteors (some missiles could be offloaded to CCAs). And have some of the fuel in CFTs or external tanks. It’s possible that the German side was willing to accept some of these trade offs, but only half heartedly, and would be happier with a larger airframe.