What is the diameter of the nozzle of Trent 1000? I am researching how much force is needed to divert the thrust of a Boeing 787 on its service ceiling of 13,100 meters and at a cruising speed of 913 km/h (data found on Wikipedia). 

As I would like to fit a diverter to it, what is the diameter of the nozzle of Trent 1000 engine?
It is mentioned here that the fan diameter is about 111-112 inches. So the nozzle must be smaller than that as the engine assembly narrows at its rear end.

This PDF (p.5) shows a diagram of the exhaust nozzle of RR Trent 1000 measuring the diameter as 63 inches. This is the only reference I could find.