Regression characteristics of the cylindrical multiport grain in hybrid rockets

Journal of Propulsion and Power

Volumn 29, Issue 3, 2013, Pages 573-581

  Kim, Soojong ^a,d   Lee, Jungpyo ^b,e   Moon, Heejang ^b,f   Kim, Jinkon ^b,f   Sung, Honggye ^b,f   Kwon, Oh Chae ^c,g  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Hankuk Aviation University   (South Korea)

^c Sungkyunkwan University   (South Korea)

^d Faculty of Aerospace Engineering   (Israel)

^e Department of Aerospace and Mechanical Engineering ^*  (South Korea)

^f School of Aerospace and Mechanical Engineering   (South Korea)

^g School of Mechanical Eng   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

FUELS; POLYESTERS; POLYETHYLENES; ROCKETS;

BURNING EFFECTS; CHAMBER PRESSURE; COMBUSTION CHARACTERISTICS; DESIGN PARAMETERS; EXPERIMENTAL RESEARCH; GEOMETRICAL CONFIGURATIONS; HYBRID ROCKET MOTORS; MERGING EFFECTS;

REGRESSION ANALYSIS;

EID: 84878279643     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.B34619     Document Type: Article

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