Development of generic algorithm in wheel-typed hybrid rocket grain design for performance estimation
Hybrid rockets are featured by restarting capability, increased safety, high performance and moderate cost. These combined unique characteristics pose then as prominent candidates to replace solid rockets in tactical missiles and launch vehicles in the near future. However, the behavior of hybrid...
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2012
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| Online Access: | http://irep.iium.edu.my/43911/ http://irep.iium.edu.my/43911/ http://irep.iium.edu.my/43911/1/2012-Development_of_Generic_Algorithm_in_Wheel-typed_Hybrid_Rocket.pdf http://irep.iium.edu.my/43911/4/IBMC_2014Fullproceeding.pdf |
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iium-439112015-07-21T04:59:44Z http://irep.iium.edu.my/43911/ Development of generic algorithm in wheel-typed hybrid rocket grain design for performance estimation Kafafy, Raed Azami, Muhammad Hanafi Idres, Moumen Zaharim, Azami Sopian, Kamaruzaman TJ Mechanical engineering and machinery Hybrid rockets are featured by restarting capability, increased safety, high performance and moderate cost. These combined unique characteristics pose then as prominent candidates to replace solid rockets in tactical missiles and launch vehicles in the near future. However, the behavior of hybrid rockets is not fully understood, with issues specifically related to combustion instability and lowered regression rate. To investigate the characteristics of hybrid rocket performance we develop generic algorithm code. This script may serve as a valuable teaching resource in hybrid rocket motor design. This paper uses Hydroxyl Terminated Polybutadiene (HTPB) as a solid fuel and liquid oxygen as an oxidizer for evaluation purposes. Later, we introduce the results of the preliminary design and performance analysis of the hybrid rocket system. An interior ballistic model was used for the analysis of hybrid rocket performance. MATLAB® environment was used to develop the design and performance analysis codes, and visualize the temporal variation of performance characteristics. 2012-12-31 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/43911/1/2012-Development_of_Generic_Algorithm_in_Wheel-typed_Hybrid_Rocket.pdf application/pdf en http://irep.iium.edu.my/43911/4/IBMC_2014Fullproceeding.pdf Kafafy, Raed and Azami, Muhammad Hanafi and Idres, Moumen and Zaharim, Azami and Sopian, Kamaruzaman (2012) Development of generic algorithm in wheel-typed hybrid rocket grain design for performance estimation. In: Advances in Environment, Computational Chemistry and Bioscience, 29-31 Dec 2012, Montreux, Switzerland . http://www.wseas.org/wseas/cms.action?id=2514 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English English |
| topic |
TJ Mechanical engineering and machinery |
| spellingShingle |
TJ Mechanical engineering and machinery Kafafy, Raed Azami, Muhammad Hanafi Idres, Moumen Zaharim, Azami Sopian, Kamaruzaman Development of generic algorithm in wheel-typed hybrid rocket grain design for performance estimation |
| description |
Hybrid rockets are featured by restarting capability, increased safety, high performance and
moderate cost. These combined unique characteristics pose then as prominent candidates to replace solid
rockets in tactical missiles and launch vehicles in the near future. However, the behavior of hybrid rockets
is not fully understood, with issues specifically related to combustion instability and lowered regression
rate. To investigate the characteristics of hybrid rocket performance we develop generic algorithm code.
This script may serve as a valuable teaching resource in hybrid rocket motor design. This paper uses
Hydroxyl Terminated Polybutadiene (HTPB) as a solid fuel and liquid oxygen as an oxidizer for evaluation
purposes. Later, we introduce the results of the preliminary design and performance analysis of the hybrid
rocket system. An interior ballistic model was used for the analysis of hybrid rocket performance.
MATLAB® environment was used to develop the design and performance analysis codes, and visualize the
temporal variation of performance characteristics. |
| format |
Conference or Workshop Item |
| author |
Kafafy, Raed Azami, Muhammad Hanafi Idres, Moumen Zaharim, Azami Sopian, Kamaruzaman |
| author_facet |
Kafafy, Raed Azami, Muhammad Hanafi Idres, Moumen Zaharim, Azami Sopian, Kamaruzaman |
| author_sort |
Kafafy, Raed |
| title |
Development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| title_short |
Development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| title_full |
Development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| title_fullStr |
Development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| title_full_unstemmed |
Development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| title_sort |
development of generic algorithm in wheel-typed hybrid rocket
grain design for performance estimation |
| publishDate |
2012 |
| url |
http://irep.iium.edu.my/43911/ http://irep.iium.edu.my/43911/ http://irep.iium.edu.my/43911/1/2012-Development_of_Generic_Algorithm_in_Wheel-typed_Hybrid_Rocket.pdf http://irep.iium.edu.my/43911/4/IBMC_2014Fullproceeding.pdf |
| first_indexed |
2023-09-18T21:02:29Z |
| last_indexed |
2023-09-18T21:02:29Z |
| _version_ |
1777410715561230336 |