Volume 39, Issue 6 pp. 859-865
Full Paper

Regression Rate Studies of Paraffin Wax-HTPB Hybrid Fuels Using Swirl Injectors

Rakesh Sakote

Rakesh Sakote

Department of Space Engineering & Rocketry, Birla Institute of Technology, Mesra, Ranchi-835215, India

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Narendra Yadav

Corresponding Author

Narendra Yadav

Department of Space Engineering & Rocketry, Birla Institute of Technology, Mesra, Ranchi-835215, India

Department of Space Engineering & Rocketry, Birla Institute of Technology, Mesra, Ranchi-835215, IndiaSearch for more papers by this author
Srinibas Karmakar

Srinibas Karmakar

Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur-721302, India

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Puran Chand Joshi

Puran Chand Joshi

Department of Space Engineering & Rocketry, Birla Institute of Technology, Mesra, Ranchi-835215, India

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Ashwini Kumar Chatterjee

Ashwini Kumar Chatterjee

Department of Space Engineering & Rocketry, Birla Institute of Technology, Mesra, Ranchi-835215, India

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First published: 28 May 2014
Citations: 16

Abstract

Studies on the regression rates of three compositions of paraffin wax-HTPB hybrid fuel grains in a stream of gaseous oxygen using two different swirl injectors at a fixed injection pressure were carried out. It was found that the regression rate in the hybrid fuel increases with increasing paraffin wax percentage, which may be attributed to melt-flow effects. The local regression rates, average regression rates, fuel mass consumption rates, and total mass fluxes for the hybrid fuels were found to be dependent on the swirl injector configuration. All three hybrid fuels were characterized by scanning electron microscopy (SEM). Furthermore, the thermal stability and thermal degradation behavior of the hybrid fuels were investigated by DTA/TGA techniques.

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