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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Main Authors: Krishnan, S., Lee, Choong Won
Format: Conference or Workshop Item
Language:English
Published: 2008
Subjects:
Online Access:http://eprints.utm.my/7410/1/SKrishnanr2008_DevelopmentofA100-nHydrogen.pdf
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author Krishnan, S.
Lee, Choong Won
author_facet Krishnan, S.
Lee, Choong Won
author_sort Krishnan, S.
collection ePrints
description 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.
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spelling utm.eprints-74102017-09-07T03:38:29Z http://eprints.utm.my/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/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.
spellingShingle TJ Mechanical engineering and machinery
Krishnan, S.
Lee, Choong Won
Development of a 100-n hydrogen peroxide rocket engine
title 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_short Development of a 100-n hydrogen peroxide rocket engine
title_sort development of a 100 n hydrogen peroxide rocket engine
topic TJ Mechanical engineering and machinery
url http://eprints.utm.my/7410/1/SKrishnanr2008_DevelopmentofA100-nHydrogen.pdf
work_keys_str_mv AT krishnans developmentofa100nhydrogenperoxiderocketengine
AT leechoongwon developmentofa100nhydrogenperoxiderocketengine