You do not need afterburner for takeoff, even when fully loaded. To compensate for less thrust, you must have runway length.
When I was active duty, my first jet was the F-111, which was nearly 48,000 lbs, and my second jet was the F-16 which was nearly 21,000 lbs.
F-16 max takeoff weight: 48,000 lbs
F-111 max takeoff weight: 100,000 lbs
Runway length RAF Upper Heyford: 8300 ft
Runway length MacDill AFB: 11,400 ft
There is a technical skill set involving calculating takeoff weight, baro, elevation, and runway length that resulted in how much and how long to apply afterburner, and am not going to the details here. Suffice to say that if the mission requires a certain amount of fuel, the F-16 pilot will use as much of that MacDill's 11,400 ft length as possible, and that mean judicious use of AB on takeoff. On the other hand, the Heyford F-111 pilot, with his jet fully loaded with two external fuel tanks and two nukes, will use full AB from start to fully airborne and then air refuel shortly in order to make the flight to Moscow. Usable runway length is more important than load when it comes to AB calculation.
With extreme combat conditions, as in the base is actually under bombardment, a pilot can hold brakes with AB but this is nearly as dangerous as getting hit by enemy weapons. The brakes cannot hold the jet even at %70 power, let alone at full AB, so do that long enough and the brakes will catastrophically fail. There is no 'rolling' takeoff here. The intention is to get as fast airflow speed over the wings as possible, so once the brakes are released after X seconds of AB, the jet will literally lurch/jump forward and the takeoff speed will be twice or greater than normal.