EFFECTS OF 1,3-DIFEROCENYL-1-BUTENE ON THE BURNING RATE OF COMPOSITE PROPELLANTS

 

Petrić Mirjana

Tasić Dimitrije

The study defines the effect of the content of ammonium-perchlorate fine particles, plasticizer and burning rate modifier (1,3-diferocenyl-1-butene) on the composite solid propellant burning rate and viscosity. The full factors experiment was used to estimate statistical importance of the analyzed factors effects. The effect of the aluminium particle size on these propellants burning rate was investigated.

Ključne reči: composite propellants, burning rate, 1,3-diferocenyl-1-butene, viscosity.

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