TECHNICAL MECHANICS
ISSN (Print): 1561-9184, ISSN (Online): 2616-6380

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UDC 621.455(075.8)

Technical mechanics, 2014, 4, 39- 52

ON THE STATEMENT OF PROBLEM OF OPTIMIZATION IN DESIGN PARAMETERS OF SOLID ROCKET ENGINE

Senkin V. S.

      The problem of the optimization the design parameters of the solid rocket engine as a nonlinear mathemati-cal programming problem with equality/inequality constraints is formulated. The elements of a mathematical model of the solid rocket engine and an algorithm for the determination of the configuration and overall dimen-sions of the charge with slots in the front bottom of the combustion chamber at the initial design stage are pre-sented. The structure of the optimized parameters of the solid rocket engine includes geometric parameters char-acterizing the initial charge configuration resulting in the selection of such a configuration, which will provide a required program of variations in time of a thrust performance of the engine in its operation.

solid rocket engine, design parameters, optimization

1. Alpatov A. P. Methodic support for selection of appearance, optimization of design parameters and programs of control of the launch vehicle flight (in Russian) / A. P. Alpatov, V. S. Senkin // Tekhnicheskaya Mekhanika. – 2013. – No 4. – P. 146 – 161.

2. Senkin V. S. Complex problem of design parameters and programs of control of a superlight solid rocket (in Russian) / V. S. Senkin // Tekhnicheskaya Mekhanika. – 2012. – No 2. – P. 106 – 121.

3. Alpatov A. P. Complex problem of optimization of the basic design parameters and programs of control of space rocket motion (in Russian) / A. P. Alpatov, V. S. Senkin // Tekhnicheskaya Mekhanika. – 2011. – No 4. – P. 98 – 113.

4. Senkin V. S. Optimization of the flight control and thrust optimization for cruise propulsion of a controlled rocket object (in Russian) / V. S. Senkin // Tekhnicheskaya Mekhanika. – 2000. – No 1. – P. 46 – 50.

5. Orlov B. V. Thermodynamic and Ballistic Principles of Design of Solid Rocket Engines (in Russian) / B. V. Orlov, G. Yu. Mazing. – Moscow : Mashinostroyenie, 1968. – 535 p.

6. Abugov D. I. The Theory and Design of Solid Rocket Engines (in Russian) / D. I. Abugov, V. M. Bobylev. – Moscow : Mashinostroyenie, 1987. – 271 p.

7. Razumeev V. F. Foundations of Design of Solid Ballistic Missiles (in Russian) / V. F. Razumeev, B. K. Kovalev. – Moscow : Mashinostroyenie, 1976. – 356 p.

8. Erokhin B. T. Unsteady and Quasi-Steady Operational Conditions of Solid Rocket Engines (in Russian) / B. T. Erokhin, A. M. Lipanov. – Moscow : Mashinostroyenie, 1977. – 200 p.

9. Erokhin B. T. Theoretical Principles of Design of Solid Rocket Engines (in Russian) / B. T. Erokhin. – Mashinostroyenie, 1982. – 206 p.

10. Shishkov A. A. Gas Dynamics of Powder Rocket Engines (in Russian) / A. A. Shishkov. – Moscow : Mashi-nostroyenie, 1974. – 156 p.

Copyright (©) 2014 Senkin V. S.

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