Development of a 100-n hydrogen peroxide rocket engine
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly reviewed. A detailed design-study of a laboratory scale facility of a hydrogen peroxide mono-propellant engine of 100-N thrust is presented. For the preparation of concentrated hydrogen peroxide, a...
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2008
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my.utm.74102017-09-07T03:38:29Z http://eprints.utm.my/id/eprint/7410/ Development of a 100-n hydrogen peroxide rocket engine Krishnan, S. 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 facility of a hydrogen peroxide mono-propellant engine of 100-N thrust is presented. For the preparation of concentrated hydrogen peroxide, a distillation facility has been realized. 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. 2008 Conference or Workshop Item PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/7410/1/SKrishnanr2008_DevelopmentofA100-nHydrogen.pdf Krishnan, S. and Lee, Choong Won (2008) Development of a 100-n hydrogen peroxide rocket engine. In: 2nd Regional Conference on Vehicle Engineering & Technology, 15 - 16 July 2008, Hotel Istana, Kuala Lumpur. |
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TJ Mechanical engineering and machinery Krishnan, S. Lee, Choong Won Development of a 100-n hydrogen peroxide rocket engine |
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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 facility of a hydrogen peroxide mono-propellant engine of 100-N thrust is presented. For the preparation of concentrated hydrogen peroxide, a distillation facility has been realized. 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 |
Conference or Workshop Item |
author |
Krishnan, S. Lee, Choong Won |
author_facet |
Krishnan, S. Lee, Choong Won |
author_sort |
Krishnan, S. |
title |
Development of a 100-n hydrogen peroxide rocket engine |
title_short |
Development of a 100-n hydrogen peroxide rocket engine |
title_full |
Development of a 100-n hydrogen peroxide rocket engine |
title_fullStr |
Development of a 100-n hydrogen peroxide rocket engine |
title_full_unstemmed |
Development of a 100-n hydrogen peroxide rocket engine |
title_sort |
development of a 100-n hydrogen peroxide rocket engine |
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2008 |
url |
http://eprints.utm.my/id/eprint/7410/1/SKrishnanr2008_DevelopmentofA100-nHydrogen.pdf http://eprints.utm.my/id/eprint/7410/ |
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1643644766176411648 |
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13.18916 |