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

Table 10

All parameters of a solid propellant missile.

Parameters	Initial	Conceptual optimal	Preliminary optimal
Total mass (kg)	4176	3518	3325
Range (km)	360	354.3	350.6
First cone length (mm)	548.1	556.3	560.4
Second cone length (mm)	2450.7	2463.1	2472.6
Column length (mm)	3301.2	3124.5	3064.6
Total length (mm)	6300	6143.9	6097.6
	4	8.8	9
	6	7.8435	7.9652
	109.5	131.1	134.2