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

Table 3

All interaction parameters between the discipline codes.

Indicator	Inputs	Outputs	Parameters
A	Geometry	Aerodynamics, RCS, propulsion, and mass	Cone length, column length, diameter, type of cone, type of rudder, type of inlet, and length and width of inlet
B	Aerodynamics	Trajectory	Aerodynamic coefficients, pressure center
C	RCS	Trajectory	Whole direction RCS data
D	Propulsion	Mass	Mass of engine charge, total mass of ISPR
E	Propulsion	Trajectory	Thrust, specific impulse, and flow rate
F	Propulsion	Geometry	Type of inlet, length and diameter of ISPR, and length and width of inlet
G	Mass	Trajectory	Total mass, mass center, and mass of engine charge
H	Trajectory	Aerodynamics	Mach number, angle of attack, and height
I	Trajectory	Mass	Horizontal/longitudinal/lateral overload