1	 Core_Diffuser: cost=417432.0
2	 Core: aircraftweight=1000000.0, totalfuel=250000.0, M_in=0.7, TSFC=0.479431, cost=962063.0,Thrust_Takeoff_Req=125000.0, NumEngines=2.0, m_core=42.5951, BPR=25.2482, OPR=29.3432, IsentropicEfficiency_compressor=0.89, Efficiency_turbine=0.89, TurbineInletTemperature=1600.34, engine_type=turboprop
3	 Core_Nozzle: cost=85190.2
4	 Multiple_Rear_Props: cost=1428200.0
