International Journal of Aerospace Engineering

Research Article

Solid Rocket Motor Design Using Hybrid Optimization

Figure 15

Optimized grain cross section for linearly regressive CP grain.
987402.fig.0015a
(a) GL = 0 in  
987402.fig.0015b
(b) GL = 45.5 in
987402.fig.0015c
(c) GL = 92 in
987402.fig.0015d
(d) GL = 137 in