International Journal of Aerospace Engineering

Research Article

Burning Characteristics of Ammonium-Nitrate-Based Composite Propellants with a Hydroxyl-Terminated Polybutadiene/Polytetrahydrofuran Blend Binder

Figure 1

Burning rate characteristics of propellants.
378483.fig.001a
(a) AN/HTPH/PTHF1
378483.fig.001b
(b) AN/HTPH/PTHF2
378483.fig.001c
(c) AN/HTPH/PTHF3