AN- BAMO-AMMO -HMX Composite Propellants

The burning rate of the propellant is clearly increased by the addition of these catalysts. The burning rate is approximately doubled by the addition of 1 % 

Propellant Ian Ibamo-ammo Shmx (NH4)2Q207 CuQ204 

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Table 7.8 Chemical compositions of AN-(BAMO-AMMO)-HMX composite propellants with and without burning rate catalysts.

Fig. 7.63 shows plots of In burning rate versus In pressure for AN-(BAMO-AMMO)-HMX propellants with and without (NHJjCrjO and CuCi20. l i The chemical compositions of these propellants are shown in Table 7.8. 

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