1	 Core_Diffuser: cost=451711.0
2	 Core: aircraftweight=1000000.0, totalfuel=250000.0, M_in=0.7, TSFC=0.519318, cost=1042110.0,Thrust_Takeoff_Req=125000.0, NumEngines=2.0, m_core=46.0929, BPR=19.9945, OPR=29.3762, IsentropicEfficiency_compressor=0.89, Efficiency_turbine=0.89, TurbineInletTemperature=1601.33, engine_type=turboprop
3	 Core_Nozzle: cost=92185.8
4	 Single_Rear_Prop: cost=458959.0
