TY  - CONF
AU  - Živković, Saša
AU  - Filipović, Miloš
AU  - Elek, Predrag
AU  - Milinović, Momčilo
AU  - Gligorijević, Nikola
AU  - Boulahlib, Mohammed Amine
PY  - 2014
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/4593
AB  - In solid propellant rocket motor internal ballistic calculation, next coefficients, performance parameters and characteristics are required: specific impulse, discharge coefficient, thrust coefficient and propellant burning rate law. All those RM working parameters can be theoretically or semi-empirically predicted, but depends from rocket motor design and combustion products flow losses; theoretical values can be very unreliable. Correction of theoretical working parameters can be provided using experimental data, although this approach is expensive and requires necessary experimental equipment. By using corrected working parameters in internal ballistic calculation highly precise results can be achieved, and accuracy of this approach is demonstrated in two different examples.
PB  - Belgrade : Military Technical Institute
C3  - 6th International Scientific Conference – OTEH 2014, Belgrade, 9-10 October 2014
T1  - Experimental determination of rocket motor internal ballistic coefficients and performance parameters
SP  - 289-298
UR  - https://hdl.handle.net/21.15107/rcub_machinery_4593
ER  - 

@conference{
author = "Živković, Saša and Filipović, Miloš and Elek, Predrag and Milinović, Momčilo and Gligorijević, Nikola and Boulahlib, Mohammed Amine",
year = "2014",
abstract = "In solid propellant rocket motor internal ballistic calculation, next coefficients, performance parameters and characteristics are required: specific impulse, discharge coefficient, thrust coefficient and propellant burning rate law. All those RM working parameters can be theoretically or semi-empirically predicted, but depends from rocket motor design and combustion products flow losses; theoretical values can be very unreliable. Correction of theoretical working parameters can be provided using experimental data, although this approach is expensive and requires necessary experimental equipment. By using corrected working parameters in internal ballistic calculation highly precise results can be achieved, and accuracy of this approach is demonstrated in two different examples.",
publisher = "Belgrade : Military Technical Institute",
journal = "6th International Scientific Conference – OTEH 2014, Belgrade, 9-10 October 2014",
title = "Experimental determination of rocket motor internal ballistic coefficients and performance parameters",
pages = "289-298",
url = "https://hdl.handle.net/21.15107/rcub_machinery_4593"
}

Živković, S., Filipović, M., Elek, P., Milinović, M., Gligorijević, N.,& Boulahlib, M. A.. (2014). Experimental determination of rocket motor internal ballistic coefficients and performance parameters. in 6th International Scientific Conference – OTEH 2014, Belgrade, 9-10 October 2014
Belgrade : Military Technical Institute., 289-298.
https://hdl.handle.net/21.15107/rcub_machinery_4593

Živković S, Filipović M, Elek P, Milinović M, Gligorijević N, Boulahlib MA. Experimental determination of rocket motor internal ballistic coefficients and performance parameters. in 6th International Scientific Conference – OTEH 2014, Belgrade, 9-10 October 2014. 2014;:289-298.
https://hdl.handle.net/21.15107/rcub_machinery_4593 .

Živković, Saša, Filipović, Miloš, Elek, Predrag, Milinović, Momčilo, Gligorijević, Nikola, Boulahlib, Mohammed Amine, "Experimental determination of rocket motor internal ballistic coefficients and performance parameters" in 6th International Scientific Conference – OTEH 2014, Belgrade, 9-10 October 2014 (2014):289-298,
https://hdl.handle.net/21.15107/rcub_machinery_4593 .