3-D grain burnback analysis of solid propellant rocket motors: Part 2-modeling and simulations

2008-12-01
Puskulcu, G.
Ulaş, Abdullah
Determination of the grain geometry is an important step in the design of solid propellant rocket motors. The performance prediction of the solid rocket motor can be achieved easily if the burnback steps of the grain are known. fit this study, grain burnback analysis for 3-D grain geometries wits investigated. The method used was solid modeling of the propellant grain for predefined intervals of burnback. In this method, the initial grain geometry was modeled parametrically using CAD software. For every burn step, the parameters were adapted and the new gram geometry was modeled. By analyzing these geometries, burn area change of the grain geometry was obtained. Using this data and internal ballistic parameters, the performance of the solid propellant rocket motor in terms of motor pressure was achieved. The comparison between the results from this study and the results front the actual rocket motor tests shows that the procedure that was developed can be Successfully used for the preliminary design of a solid propellant rocket motor. (C) 2008 Elsevier Masson SAS. All rights reserved.
AEROSPACE SCIENCE AND TECHNOLOGY

Suggestions

3-D grain burnback analysis of solid propellant rocket motors: Part 1-ballistic motor tests
Puskulcu, G.; Ulaş, Abdullah (Elsevier BV, 2008-12-01)
The performance prediction of solid rocket motors is an important phase during the design process and it can be achieved easily if the burnback steps of the solid propellant are known. A method was developed by the authors to analyze and determine the grain burnback of solid propellants in rocket motors. To verify the predictions from the model, subscale ballistic rocket motor tests were performed in this study. An existing rocket motor was modified in terms of insulation, ignition delay, and sealing. Compo...
Ballistic design optimization of three-dimensional grains using genetic algorithms
Yücel, Osman; Aksel, Mehmet Haluk; Department of Mechanical Engineering (2012)
Within the scope of this thesis study, an optimization tool for the ballistic design of three-dimensional grains in solid propellant rocket motors is developed. The modeling of grain geometry and burnback analysis is performed analytically by using basic geometries like cylinder, cone, sphere, ellipsoid, prism and torus. For the internal ballistic analysis, a quasi-steady zero-dimensional flow solver is used. Genetic algorithms have been studied and implemented to the design process as an optimization algor...
Analysis of grain burnback and international flow in solid propellant rocket motors in 3-dimensions
Yıldırım, Cengizhan; Aksel, Mehmet Haluk; Department of Mechanical Engineering (2007)
In this thesis, Initial Value Problem of Level-set Method is applied to solid propellant combustion to find the grain burnback. For the performance prediction of the rocket motor, 0-D, 1-D or 3-D flow models are used depending on the type of thre grain configuration.
Experimental analysis on the measurement of ballistic properties of solid propellants
Cuerdaneli, S.; Ak, M. A.; Ulaş, Abdullah (2007-06-16)
Ballistic properties of solid propellants play an important role in the performance of the solid propellant rocket motors. Therefore, ballistic properties of a likely propellant should be known and provided to the design engineers. In this study, a specific AP/HTPB composite solid propellant (SCP) was examined to obtain steady-state linear burning rates as a function of pressure and propellant initial temperature, temperature sensitivity, and pressure deflagration limit (PDL). In some tests micro-thermocoup...
Three-dimensional retarding walls and flow in their vicinity
Toker, Kemal Atılgan; Aksel, Mehmet Haluk; Department of Mechanical Engineering (2004)
The performance prediction of solid propellant rocket motor depends on the calculation of internal aerodynamics of the motor through its operational life. In order to obtain the control volume, in which the solutions will be carried out, a process called أgrain burnback calculationؤ is required. During the operation of the motor, as the interface between the solid and gas phases moves towards the solid propellant in a direction normal to the surface, the combustion products are generated and added into the ...
Citation Formats
G. Puskulcu and A. Ulaş, “3-D grain burnback analysis of solid propellant rocket motors: Part 2-modeling and simulations,” AEROSPACE SCIENCE AND TECHNOLOGY, pp. 585–591, 2008, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/44221.