Design and development of a hydrogen-peroxide rocket-engine facility
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly reviewed. A detailed design-study of a laboratory scale hydrogen peroxide mono-propellant engine of 100 N thrust is presented. For the preparation of concentrated hydrogen peroxide, a distillation fa...
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Faculty of Mechanical Engineering
2010
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my.utm.70572017-10-11T01:26:32Z http://eprints.utm.my/id/eprint/7057/ Design and development of a hydrogen-peroxide rocket-engine facility Krishnan, Subramaniam Ahn, Sang-Hee Lee, Choong-Won TJ Mechanical engineering and machinery The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly reviewed. A detailed design-study of a laboratory scale hydrogen peroxide mono-propellant engine of 100 N thrust is presented. For the preparation of concentrated hydrogen peroxide, a distillation facility has been realised. Results of water analogy tests are presented. Initial firings using the concentrated hydrogen peroxide were not successful. Low environmental temperature, low contact area of the catalyst pack, and contamination in the hydrogen peroxide were considered to be the reasons. Addressing the first two points resulted in successful firing of the rocket engine Faculty of Mechanical Engineering 2010-06 Article PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/7057/1/SubramaniamKrishnan2010_DesignandDevelopmentofaHydrogenperoxide.pdf text/html en http://eprints.utm.my/id/eprint/7057/2/design-subramaniam_Jld30-Jun2010_24-36.pdf Krishnan, Subramaniam and Ahn, Sang-Hee and Lee, Choong-Won (2010) Design and development of a hydrogen-peroxide rocket-engine facility. Jurnal Mekanikal : An International Journal (30). pp. 24-36. ISSN 0127-3396 |
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TJ Mechanical engineering and machinery Krishnan, Subramaniam Ahn, Sang-Hee Lee, Choong-Won Design and development of a hydrogen-peroxide rocket-engine facility |
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The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly reviewed. A detailed design-study of a laboratory scale hydrogen peroxide mono-propellant engine of 100 N thrust is presented. For the preparation of concentrated hydrogen peroxide, a distillation facility has been realised. Results of water analogy tests are presented. Initial firings using the concentrated hydrogen peroxide were not successful. Low environmental temperature, low contact area of the catalyst pack, and contamination in the hydrogen peroxide were considered to be the reasons. Addressing the first two points resulted in successful firing of the rocket engine |
format |
Article |
author |
Krishnan, Subramaniam Ahn, Sang-Hee Lee, Choong-Won |
author_facet |
Krishnan, Subramaniam Ahn, Sang-Hee Lee, Choong-Won |
author_sort |
Krishnan, Subramaniam |
title |
Design and development of a hydrogen-peroxide rocket-engine facility
|
title_short |
Design and development of a hydrogen-peroxide rocket-engine facility
|
title_full |
Design and development of a hydrogen-peroxide rocket-engine facility
|
title_fullStr |
Design and development of a hydrogen-peroxide rocket-engine facility
|
title_full_unstemmed |
Design and development of a hydrogen-peroxide rocket-engine facility
|
title_sort |
design and development of a hydrogen-peroxide rocket-engine facility |
publisher |
Faculty of Mechanical Engineering |
publishDate |
2010 |
url |
http://eprints.utm.my/id/eprint/7057/1/SubramaniamKrishnan2010_DesignandDevelopmentofaHydrogenperoxide.pdf http://eprints.utm.my/id/eprint/7057/2/design-subramaniam_Jld30-Jun2010_24-36.pdf http://eprints.utm.my/id/eprint/7057/ |
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