Multifidelity Multidisciplinary Design Optimization of Integral Solid Propellant Ramjet Supersonic Cruise Vehicles

Table 6

Accuracy of each discipline codes.

		Low LoF	Medium LoF	High LoF
Aerodynamic		0.3769	0.4234	0.4246
RCS		0.0795 m^2	0.0832 m^2	0.0821 m^2
Propulsion		8150 N	—	8341 N
Mass		1010 kg	—	973 kg