How effective could the Mirage G8A be with 55° sweep angle? If for some reason the G8A entered production and went into a conflict
Would it worked as well as the Mirage F1 when it comes to dogfights, bombing, interception, etc?
Super Mirage G8A/ACF would have been a "F-15 class" fighter (in terms of raw performance) with less advanced aerodynamics.
The original G and G8 were MiG-23 and F-111/F-14A class, respectively.
The decision to replace US-designed TF-30s with French M53s on the G8A gave it superior engines to those of an F-14A. But let's not forget that, while on paper it should have superior raw performance in the air to an F-14A, keep in mind that it would have inferior agility and cockpit visibility, and it was very likely to get inferior weapons and avionics suite.
Speaking of Grumman, an early Grumman FX (pictured below) study showed similar characteristics to the G8A.
The G8A's 55° wing sweep would have made the aircraft unsuitable for carrier-based / short runway operations.
It would have been decent for interception, ground attack, and nuclear deterrence. Think of it as a less rugged, larger Mirage F1 (so.. F2) with Mirage 2000 tech inside.
Otherwise, it was too expensive for what it offered, and I don't think it was attractive to Dassault's usual export customers.
The later Mirage 4000 would have been a better multirole twin M53, F-15 class fighter.
Edit: small mistake pointed out by Archibald