Find at least one other similar power system from different manufacturers. Briefly list their specifications and possible images/drawings of the aircraft and power system. Find the maximum thrust, fuel consumption and other relevant data of the current Airbus A340-300 [20 %] 2. and published longest range (in your report you need demonstrate the source of your data). Using possible published data and some assumed specifications, estimate the mass flow rate and the exhaust exit velocities of the main nozzle and the bypass flow, and calculating the propulsive efficiency. [10 %] 3. For your design, using your power system parameters, thrust requirement during taking off, cruise, landing and taxiing, estimate the max range of your aircraft. You need find the optimal bypass ratio for optimizing the fuel consumption of your design. [40 %] 4. Based on your design and proposed operating parameters, analyse the ideal cycle of your gas turbine engine, and find the cycle efficiency of your design. [20 %] 5. Estimate the total CO2 emissions based on the max aircraft range [10 %]