There
are certification rules which address elements of this - for example 25.735(f) discusses "return to land" failure scenarios in the context of brake KE:
(Guidance material)
The critical landing weight for this condition is the maximum take-off weight, less fuel burned and jettisoned during a return to the departure airfield. A 30-minute flight should be assumed, with 15 minutes of active fuel jettisoning if equipped with a fuel jettisoning system.
Since part 25 doesn't explicitly require consideration of contaminated runways during design, it would be surprised if the contaminated case were explicitly or consistently addressed for such a scenario, though.