Conceptual Aircraft Empennage Design Based on Multidisciplinary Design Optimization Approach

Table 4

Calculated component mass as compared to reference [15].

	Calculated (kg)	Reference (kg)	Difference (%)
MTOW	75985.7	77000.0	1.32
OWE	42059.2	42092.0	0.08
Block fuel	14609.2	14733.0	0.84
Wing mass	8165.3	8097.0	-0.84
HTP mass	676.9	682.0	0.75
VTP mass	538.5	522.0	-3.17