Research Article
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 |
|
|