Mathematical Modelling of In-Chamber Processes in Hydrocombined Propellant Solid Rocket Motors

Authors

  • Nikolai A. Obukhov National Rocket Centre, Miass , Russia
  • Sergei A. Bitkin National Rocket Centre, Miass ,Russia
  • Alexander B. Vorozhtsov Tomsk State University, Tomsk, Russia

DOI:

https://doi.org/10.14429/dsj.48.3956

Keywords:

Hydrocombined propellant, Commercial rockets, Combustion chamber, Solid propellants

Abstract

The special conditions of employment of commercial rockets in the sea environment has opened up new possibilities of improving motor performance. The interesting method suggests supplying water into the running motor. This paper reports the calculations and experiments carried out with solid propellant model setups. The results prove the validity of the proposed method and allow the refinement of calculation techniques for the prediction of solid rocket motor performance characteristics. The serviceability of the solid propellant charges working in combination with water is demonstrated. A mathematical model is proposed for the operation of a hydrocombined propellant motor with water and powdered additives applied to the combustion chamber."

Author Biographies

Nikolai A. Obukhov, National Rocket Centre, Miass , Russia

National Rocket Centre, Miass ,Russia

Sergei A. Bitkin, National Rocket Centre, Miass ,Russia

National Rocket Centre, Miass ,Russia

Alexander B. Vorozhtsov, Tomsk State University, Tomsk, Russia

Tomsk State University, Tomsk, Russia

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Published

2013-01-01

How to Cite

Obukhov, N. A., Bitkin, S. A., & Vorozhtsov, A. B. (2013). Mathematical Modelling of In-Chamber Processes in Hydrocombined Propellant Solid Rocket Motors. Defence Science Journal, 48(4), 331–336. https://doi.org/10.14429/dsj.48.3956

Issue

Section

Aeronautical Systems