Initial temperature influence on the powder speed combustion in the high pressure range

Author:

Tančić Ljubiša

Publisher

Centre for Evaluation in Education and Science (CEON/CEES)

Reference7 articles.

1. Timnat, Y. M.: Advanced Chemical Rocket Propulsion, Department of Aeronautical Engineering and Space Research Institute, Technion-Israel Institute of Technology, Haifa, Israel, 1987.;

2. Kubota, N.: Survey of Rocket Propellants and Their Combustion Characteristic, Japan Defense Agency, Tokyo, Japan, 1982.;

3. Sepelev, Yu. G., Fogelzang, A. E., Denisjuk, A. P., Demidov, A. E.: Vlijanije načalnoj temperaturi na skorost gorenija ballistitnih porohov v oblasti visokoga davlenija, Fizika gorenija i vzriva, br. 4/90, Moskva, 1990.;

4. Cvetković, M.: Unutrašnja balistika, lekclje, TSC VTA KoV JNA, Zagreb, 1981.;

5. Shechadri, T. S., Jain, V. K.: Propellant Gas Phase Chemical Kinetics, Department of Aerospace Engineering, Indian Institute of Science, Bangalore, Propellants, Explosives, Pyrotechnics 14, 1989. strana 193 do 198.;

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