Theoretical thermodynamic combustion properties of composite propellants

• Autorzy: Florczak B.
• Języki publikacji: EN

Abstrakty

EN

This paper is a brief thermodynamic calculation (ICT Thermodynamic Code) of the thermochemical properties of metallized solid composite propellants (binder, Al and AP, ADN, HMX, CL-20, NTO, TNAZ, FOX-7). The calculations were performed for rocket equilibrium at 7.0 MPa, considering an adiabatic through a nozzle in one–dimensional flow at chemical equilibrium and with an expansion ratio 70:1. The calculations: flame temperature, molecular weight of combustion products, specific impulse and composition of combustion products were performed for propellant formulations on the base binder (HTPB, HMDI and DOA) with solid loading above 60%.

Słowa kluczowe

EN

thermodynamic properties; nitro compounds

• Wydawca: Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
• Czasopismo: Materiały Wysokoenergetyczne
• Rocznik: 2009
• Tom: T. 1
• Strony: 95--106
• Opis fizyczny: Bibliogr. 13 poz., rys., tab.

Twórcy

autor

Florczak B.

• Institute of Industrial Organic Chemistry, 6 Annopol str., 03-236 Warszawa, PL

Bibliografia

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