Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives

Hybrid Rocket Motor (HRM) has a critical weakness that impacts performance because of low regression rate. Due to this, extensive investigation has been done on the end-burning hybrid rocket (EBHR) to enhance the regression rate. Analytical studies were conducted on the EBHR to model the internal ba...

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Published in:AIAA SciTech Forum and Exposition, 2023
Main Author: Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
Format: Conference paper
Language:English
Published: American Institute of Aeronautics and Astronautics Inc, AIAA 2023
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85198990539&doi=10.2514%2f6.2023-0893&partnerID=40&md5=3e83bc03c4b8e90bfec4dfceb442abce
id 2-s2.0-85198990539
spelling 2-s2.0-85198990539
Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
2023
AIAA SciTech Forum and Exposition, 2023


10.2514/6.2023-0893
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85198990539&doi=10.2514%2f6.2023-0893&partnerID=40&md5=3e83bc03c4b8e90bfec4dfceb442abce
Hybrid Rocket Motor (HRM) has a critical weakness that impacts performance because of low regression rate. Due to this, extensive investigation has been done on the end-burning hybrid rocket (EBHR) to enhance the regression rate. Analytical studies were conducted on the EBHR to model the internal ballistic flow field in the combustion port at different initial configurations. The present investigation is focused on single port EBHR, paraffin wax doped with high entropy additives (HEA), and gas oxygen as the fuel and oxidiser, respectively. Three different HRM configurations will be investigated to compare the enhancement of regression rate: conventional HRM, EBHR, and EBHR with additives. The experimental work was conducted using FeCoNiAl(0.1-x)BxSi doped in paraffin wax for end-burning static firing. HEA contributes to an increase of 1.11% to the regression rate, 12.27% to the thrust, and 12.16% to the specific impulse of the HRM compared to pure paraffin wax fuel. EBHR has an overall lower performance than conventional HRM. The results show an increase of 44.32% and 52.75% in regression rate for fuel with 5% and 7% HEA concentrations, respectively, compared to the baseline of 3%. The mass of the fuel has the most impact on the regression rate, with an increase of 104.4% for 50% more fuel mass compared to the baseline. However, the HRM with the highest specific impulse is the one with a rise of 22.62% mass flux as compared to the baseline. © 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
American Institute of Aeronautics and Astronautics Inc, AIAA

English
Conference paper

author Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
spellingShingle Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
author_facet Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
author_sort Sabri M.E.E.; Roslan M.A.Q.; Azami M.H.; Salleh Z.
title Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
title_short Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
title_full Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
title_fullStr Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
title_full_unstemmed Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
title_sort Regression Rate End-Burning Hybrid Rocket Motor Doped with High Entropy Metallic Additives
publishDate 2023
container_title AIAA SciTech Forum and Exposition, 2023
container_volume
container_issue
doi_str_mv 10.2514/6.2023-0893
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85198990539&doi=10.2514%2f6.2023-0893&partnerID=40&md5=3e83bc03c4b8e90bfec4dfceb442abce
description Hybrid Rocket Motor (HRM) has a critical weakness that impacts performance because of low regression rate. Due to this, extensive investigation has been done on the end-burning hybrid rocket (EBHR) to enhance the regression rate. Analytical studies were conducted on the EBHR to model the internal ballistic flow field in the combustion port at different initial configurations. The present investigation is focused on single port EBHR, paraffin wax doped with high entropy additives (HEA), and gas oxygen as the fuel and oxidiser, respectively. Three different HRM configurations will be investigated to compare the enhancement of regression rate: conventional HRM, EBHR, and EBHR with additives. The experimental work was conducted using FeCoNiAl(0.1-x)BxSi doped in paraffin wax for end-burning static firing. HEA contributes to an increase of 1.11% to the regression rate, 12.27% to the thrust, and 12.16% to the specific impulse of the HRM compared to pure paraffin wax fuel. EBHR has an overall lower performance than conventional HRM. The results show an increase of 44.32% and 52.75% in regression rate for fuel with 5% and 7% HEA concentrations, respectively, compared to the baseline of 3%. The mass of the fuel has the most impact on the regression rate, with an increase of 104.4% for 50% more fuel mass compared to the baseline. However, the HRM with the highest specific impulse is the one with a rise of 22.62% mass flux as compared to the baseline. © 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
publisher American Institute of Aeronautics and Astronautics Inc, AIAA
issn
language English
format Conference paper
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