Experimental investigation of erosion rate of insulation materials using hybrid rockets

Thermal insulation is essential to protect the exposed surface from high-temperature and high heat flux situations. The selection of suitable insulation materials plays a crucial role in determining rocket performance. Testing of these materials for their erosion rate is possible only if the require...

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Main Authors: Phaninder Reddy Vaka, Nikunj Rathi, P.A. Ramakrishna
Format: Article
Language:English
Published: KeAi Communications Co. Ltd. 2021-12-01
Series:FirePhysChem
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2667134421000572
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author Phaninder Reddy Vaka
Nikunj Rathi
P.A. Ramakrishna
author_facet Phaninder Reddy Vaka
Nikunj Rathi
P.A. Ramakrishna
author_sort Phaninder Reddy Vaka
collection DOAJ
description Thermal insulation is essential to protect the exposed surface from high-temperature and high heat flux situations. The selection of suitable insulation materials plays a crucial role in determining rocket performance. Testing of these materials for their erosion rate is possible only if the required high heat flux conditions are met. This testing is more amenable with hybrid rockets than with solid and liquid rockets. The present study is to examine the erosion of few materials using a lab-scale hybrid rocket motor. The heat flux experienced by the fuel surface is measured using slug type calorimeter. Erosion rates of 4 different materials under these heat flux conditions are reported in the paper. A correlation is presented in the paper between erosion rate and heat flux for the materials tested.
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spelling doaj.art-5a24cd86b84d4bfeba0a136c50fd889c2022-12-27T04:40:47ZengKeAi Communications Co. Ltd.FirePhysChem2667-13442021-12-0114222230Experimental investigation of erosion rate of insulation materials using hybrid rocketsPhaninder Reddy Vaka0Nikunj Rathi1P.A. Ramakrishna2Corresponding author.; Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, IndiaDepartment of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, IndiaDepartment of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, IndiaThermal insulation is essential to protect the exposed surface from high-temperature and high heat flux situations. The selection of suitable insulation materials plays a crucial role in determining rocket performance. Testing of these materials for their erosion rate is possible only if the required high heat flux conditions are met. This testing is more amenable with hybrid rockets than with solid and liquid rockets. The present study is to examine the erosion of few materials using a lab-scale hybrid rocket motor. The heat flux experienced by the fuel surface is measured using slug type calorimeter. Erosion rates of 4 different materials under these heat flux conditions are reported in the paper. A correlation is presented in the paper between erosion rate and heat flux for the materials tested.http://www.sciencedirect.com/science/article/pii/S2667134421000572Hybrid rocketsErosion rateFuel surface heat fluxInsulation materialsWax based hybrid rockets
spellingShingle Phaninder Reddy Vaka
Nikunj Rathi
P.A. Ramakrishna
Experimental investigation of erosion rate of insulation materials using hybrid rockets
FirePhysChem
Hybrid rockets
Erosion rate
Fuel surface heat flux
Insulation materials
Wax based hybrid rockets
title Experimental investigation of erosion rate of insulation materials using hybrid rockets
title_full Experimental investigation of erosion rate of insulation materials using hybrid rockets
title_fullStr Experimental investigation of erosion rate of insulation materials using hybrid rockets
title_full_unstemmed Experimental investigation of erosion rate of insulation materials using hybrid rockets
title_short Experimental investigation of erosion rate of insulation materials using hybrid rockets
title_sort experimental investigation of erosion rate of insulation materials using hybrid rockets
topic Hybrid rockets
Erosion rate
Fuel surface heat flux
Insulation materials
Wax based hybrid rockets
url http://www.sciencedirect.com/science/article/pii/S2667134421000572
work_keys_str_mv AT phaninderreddyvaka experimentalinvestigationoferosionrateofinsulationmaterialsusinghybridrockets
AT nikunjrathi experimentalinvestigationoferosionrateofinsulationmaterialsusinghybridrockets
AT paramakrishna experimentalinvestigationoferosionrateofinsulationmaterialsusinghybridrockets