Energies 2011, 4(10), 1779-1839; doi:10.3390/en4101779
Article

Polymer Combustion as a Basis for Hybrid Propulsion: A Comprehensive Review and New Numerical Approaches

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Received: 28 July 2011; in revised form: 11 October 2011 / Accepted: 12 October 2011 / Published: 24 October 2011
(This article belongs to the Special Issue Combustion for Aerospace Propulsion)
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Abstract: Hybrid Propulsion is an attractive alternative to conventional liquid and solid rocket motors. This is an active area of research and technological developments. Potential wide application of Hybrid Engines opens the possibility for safer and more flexible space vehicle launching and manoeuvring. The present paper discusses fundamental combustion issues related to further development of Hybrid Rockets. The emphasis is made on the two aspects: (1) properties of potential polymeric fuels, and their modification, and (2) implementation of comprehensive CFD models for combustion in Hybrid Engines. Fundamentals of polymeric fuel combustion are discussed. Further, steps necessary to accurately describe their burning behaviour by means of CFD models are investigated. Final part of the paper presents results of preliminary CFD simulations of fuel burning process in Hybrid Engine using a simplified set-up.
Keywords: hybrid propulsion; polymeric fuels; combustion; computational fluid dynamics
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MDPI and ACS Style

Novozhilov, V.; Joseph, P.; Ishiko, K.; Shimada, T.; Wang, H.; Liu, J. Polymer Combustion as a Basis for Hybrid Propulsion: A Comprehensive Review and New Numerical Approaches. Energies 2011, 4, 1779-1839.

AMA Style

Novozhilov V, Joseph P, Ishiko K, Shimada T, Wang H, Liu J. Polymer Combustion as a Basis for Hybrid Propulsion: A Comprehensive Review and New Numerical Approaches. Energies. 2011; 4(10):1779-1839.

Chicago/Turabian Style

Novozhilov, Vasily; Joseph, Paul; Ishiko, Keiichi; Shimada, Toru; Wang, Hui; Liu, Jun. 2011. "Polymer Combustion as a Basis for Hybrid Propulsion: A Comprehensive Review and New Numerical Approaches." Energies 4, no. 10: 1779-1839.


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