I am looking for the approximate thrust of a C-130J Hercules under ISA sea level conditions. Also the efficiency of its propeller would be of help.
An answer to this question would really help my calculations for an assignment, so I don't have to guess values. If you could direct me to your sources as well, that would be highly appreciated.
The C-130J is equipped with Rolls Royce AE-2100 D3 engines and the propellers would be the 6-bladed Dowty R391.