Wouldn't the conops dictate what they want from the plane? Along with the budget given to the builder who puts forward if it has 1,2 or 3 engines, If the PAK budget alowed the development tech to have the needed thrust in a single engine, it would have one, as I see it.
The conops might include vignettes of typical utility and state
must be able to fly A-B in AA combat load config to a range of nn kilometres with 60% of mission set over green/grey/blue water
powerplant must have nn hours ave MTBF
powerplant must be able to run for nn hours before major pulldown
powerplant must be able to maintained to Lev xxx within existing maint contracts
vendors can come back with a response that addresses that but via different solution sets
some might offer more fuel efficient engines to achieve range
some might offer larger tanks to achieve range
some might offer tech where platform dry weight is reduced substantially and power to weight/thrust increases accordingly
some might recess weapons to minimise drag
some might offer spare powerplants on a 24h turnaround and imply reduced downtime
some might offer to set up hi-lev maint in country to reduce downtime and increase support autonomy
some might offer multiple engines as an increase in time on station solution
etc etc
I've done some aircraft evals offshore, and generally speaking. multi-engined platforms have ugly maint and through life costs - even if the powerplant unit price is bought down due to volume benefits, one has to consider that close to 50% of your absolute costs will be eaten by maint
the arguments for multi over singles don't stand up to the stats though - remember that the most reliable single engine fighter in the world is the viper. raw stats eat marketing stats on any day of the week.
that includes availability
accidents - across various measurement vectors
overall hours
across various engine types
manufacturers can't BS on engine data as every airforce maintains their own data - irrespective of the nature of the contract