Question: We are analyzing a solid rocket motor ( aluminized ammonium perchlorate composite, chamber pressure 1 0 0 0 psia ) , using an internal burning

We are analyzing a solid rocket motor (aluminized ammonium perchlorate composite, chamber pressure 1000 psia), using an internal burning tube design. Use Table 5-7.
1. During operation, the motor experiences a 1L combustion instability mode at 392 Hz between the motor casing head and the nozzle throat. Calculate the length of the motor between those two points.
We are analyzing a solid rocket motor (

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