Research on Optimization of Aircraft Climb Trajectory considering Environmental Impact

Table 2

Flight parameter variation with minimum fuel consumption and total temperature rise.

Condition	(kt)	(kg)	(×10^−12°C)	(kg)	(kg)
Total minimum	260	1238.554	1.8912	26.511	3907.638
Total minimum	280	1247.401	1.8781	27.224	3935.552