Study of Burn Rate Suppressants in AP‐Based Composite Propellants

Vishwas Govindrao Ghorpade, Abhijit Dey, Lalita Jawale, Amarnath Madiwal Kotbagi, Arvind Kumar, Manoj Kumar Gupta

Propellants Explosives Pyrotechnics · 2010 · 33 citations · 2 references

Concepts

Abstract

Abstract A number of composite propellant compositions based on various burn rate suppressants were formulated and studied with the aim to select a suitable burn rate suppressant for reducing the burn rate of the basic propellant composition. Theoretical properties of the compositions were computed by using NASA CEC‐71 program and the burn rate performance was evaluated. In addition, sensitivity, thermal, and mechanical properties of the compositions were also evaluated. The composition containing 60% AP, 10% Al, 20% binder, and 10% burn rate suppressant (melamine) was insensitive to friction and impact (28.8 kg and 0.56 m) and showed 90% weight loss. The formulation was found to be relatively superior.

References

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