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The design of a kerosene turbopump for a South African commercial launch vehicle

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dc.contributor.author Snedden, Glen C
dc.contributor.author Smyth, J
dc.contributor.author Bindon, J
dc.contributor.author Brooks, M
dc.contributor.author Smith, G
dc.date.accessioned 2013-01-30T09:08:11Z
dc.date.available 2013-01-30T09:08:11Z
dc.date.issued 2012-08
dc.identifier.citation Snedden, GC, Smyth, J, Bindon, J, Brooks, M and Smith, G. 2012. The design of a kerosene turbopump for a South African commercial launch vehicle. In: 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Altlanta, Georgia, USA, 30 July - 1 August 2012 en_US
dc.identifier.uri http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3763
dc.identifier.uri http://hdl.handle.net/10204/6500
dc.description 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Altlanta, Georgia, USA, 30 July - 1 August 2012. Published in AIAA 2012. en_US
dc.description.abstract A South African turbopump design capability would be critical to any future indigenous commercial launch capacity. This paper describes the initial work being done at the University of KwaZulu-Natal (UKZN) to design a kerosene turbopump for a hypothetical commercial launch vehicle capable of inserting 50-500kg payloads into 500km sun synchronous orbit. A preliminary design is presented with the focus on the turbopump impeller geometry and its predicted performance. en_US
dc.language.iso en en_US
dc.publisher AIAA 2012 en_US
dc.relation.ispartofseries Workflow;9732
dc.subject Turbopump design en_US
dc.subject University of KwaZulu-Natal en_US
dc.subject Kerosene turbopump en_US
dc.subject Sun synchronous orbit en_US
dc.subject Turbopump impeller geometry en_US
dc.subject Commercial launch vehicle en_US
dc.title The design of a kerosene turbopump for a South African commercial launch vehicle en_US
dc.type Conference Presentation en_US
dc.identifier.apacitation Snedden, G. C., Smyth, J., Bindon, J., Brooks, M., & Smith, G. (2012). The design of a kerosene turbopump for a South African commercial launch vehicle. AIAA 2012. http://hdl.handle.net/10204/6500 en_ZA
dc.identifier.chicagocitation Snedden, Glen C, J Smyth, J Bindon, M Brooks, and G Smith. "The design of a kerosene turbopump for a South African commercial launch vehicle." (2012): http://hdl.handle.net/10204/6500 en_ZA
dc.identifier.vancouvercitation Snedden GC, Smyth J, Bindon J, Brooks M, Smith G, The design of a kerosene turbopump for a South African commercial launch vehicle; AIAA 2012; 2012. http://hdl.handle.net/10204/6500 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Snedden, Glen C AU - Smyth, J AU - Bindon, J AU - Brooks, M AU - Smith, G AB - A South African turbopump design capability would be critical to any future indigenous commercial launch capacity. This paper describes the initial work being done at the University of KwaZulu-Natal (UKZN) to design a kerosene turbopump for a hypothetical commercial launch vehicle capable of inserting 50-500kg payloads into 500km sun synchronous orbit. A preliminary design is presented with the focus on the turbopump impeller geometry and its predicted performance. DA - 2012-08 DB - ResearchSpace DP - CSIR KW - Turbopump design KW - University of KwaZulu-Natal KW - Kerosene turbopump KW - Sun synchronous orbit KW - Turbopump impeller geometry KW - Commercial launch vehicle LK - https://researchspace.csir.co.za PY - 2012 T1 - The design of a kerosene turbopump for a South African commercial launch vehicle TI - The design of a kerosene turbopump for a South African commercial launch vehicle UR - http://hdl.handle.net/10204/6500 ER - en_ZA


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