CPC F02K 9/38 (2013.01) [F02K 9/346 (2013.01); F42B 1/028 (2013.01)] | 20 Claims |
1. A rocket motor comprising:
a casing;
a solid propellent; and
an energetic material between the solid propellent and the casing;
wherein the energetic material is configured to burn along with the solid propellent to produce thrust in the rocket motor;
wherein the energetic material is configured to be capable of detonation to rupture the casing; and
wherein the energetic material is part of a linear shaped charge.
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