Optimized variables cruising pressure altitude pcruise and speed correction factor α with corresponding results of the time of flight and fuel burn for different objectives of optimization.

Table 2: Optimized variables cruising pressure altitude p_cruise and speed correction factor α with corresponding results of the time of flight and fuel burn for different objectives of optimization.

Objective	Parameter	MD-11F	B777F
Min. time	pcruise	210 hPa	220 hPa
	α	1.12	1.10
	Time of flight	19461s	19667s
	Fuel burn	44852 kg	44715 kg
Min. fuel burn	pcruise	220 hPa	240 hPa
	α	0.94	1.01
	Time of flight	19537s	20403s
	Fuel burn	44816 kg	41151 kg