I'm doing some estimations of weight and thrust loading for a college project, and in the formula below the landing distance is not a variable, but should be estimated using similar aircraft and usual runways. (There is also a formula for landing with the same problem)
The similar aircrafts are 18-21 meter self-launching motor gliders like DG-505MB, DG-1001M or ASG 32 Mi (but with absolutely no data I have now, information about any other gliders would be appreciated as well).
The only thing I've found was that European Regulations CS-22 allow motor gliders a maximum takeoff distance of 500 metres.
Source; T.C.Cork, Design of Aircraft