• Title/Summary/Keyword: O/F비k

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A Study on Relation between the Fuel Mass Flux and the Oxidizer Mass Flux with the Initial Port Diameter in Hybrid Rocket (하이브리드 로켓에서의 초기 포트직경을 고려한 산화제 유속과 고체연료 유속과의 관계에 관한 연구)

  • Lee, Jung-Pyo;Cho, Sung-Bong;Yoon, Sang-Kyu;Park, Su-Hayng;Song, Na-Young;Kim, Gi-Hun;Cho, Jung-Tae;Sung, Hong-Gye;Moon, Hee-Jang;Kim, Jin-Kon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.243-247
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    • 2007
  • Fuel mass flux was experienced with a function of the oxidizer mass flux using initial port area of solid fuel, in stead of regression rate correlation which shows combustion characteristic in hybrid propulsion. The burning rate could be easily obtained by using the oxidizer mass flux of initial port area without iteration, and fuel configuration could be designed simply. In this experiments PE was used as fuel, COX was used as oxidizer. A variation of mass flux of solid fuel with port area is considered by changing the burning time. In the case of approximate 0.5 for an exponent of oxidizer mass flux, using the fuel mass flux correlation is more suitable than regression rate correlation in hybrid propulsion.

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