REPUBLIC OF SERBIA MINISTRY OF DEFENCE
MINISTRY OF DEFENCE Material Resources Sector Defensive Technologies Department
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experimental determination of rocket motor internal ballistic coefficients and performance parameters
Military Technical Institute, Belgrade, vti@vti.vs.rs MILOŠ FILIPOVIĆ Faculty, University of Novi Pazar, Novi Pazar, mfilipovic@np.ac.rs PREDRAG ELEK Faculty of Mechanical Engineering, University of Belgrade, Belgrade, pelek@mas.bg.ac.rs MOMČILO MILINOVIĆ Faculty of Mechanical Engineering, University of Belgrade, Belgrade, mmilinovic@mas.bg.ac.rs NIKOLA GLIGORIJEVIĆ Military Technical Institute, Belgrade, nikola.gligorijevic@gmail.com MOHAMMED AMINE BOULAHLIB Military Academy, University of Defense, Belgrade, vti@vti.vs.rs
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. Keywords: rocket motor, internal ballistic calculation, coefficients, performances, measuring.
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