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The maximum thrust of the afterburner thruster for one engine should be AB_Thrust - dry_thrust.
Real afterburners also start in rapid stages, but for most observers, instantly at full after burner thrust is OK.
Maybe you should constantly recalculate maximum afterburner and dry thrust depending on air speed and air density for more realism. A higher speed slightly increases thrust, a higher altitude lowers it. The thrust given for the engine are usually static test results, sea-level pressure, zero velocity.
Real afterburners also start in rapid stages, but for most observers, instantly at full after burner thrust is OK.
Maybe you should constantly recalculate maximum afterburner and dry thrust depending on air speed and air density for more realism. A higher speed slightly increases thrust, a higher altitude lowers it. The thrust given for the engine are usually static test results, sea-level pressure, zero velocity.