The proceedings of the JSME annual meeting
Online ISSN : 2433-1325
2008.5
Session ID : 4042
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4042 Structural design of K-class hybrid rockets in Tokai University
Toshiyuki ITOHumio TOHYAMAKyouiti NAKASHINO
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Abstract

K-class hybrid rockets are usually retrieved with parachutes. At the parachute opening phase, the rocket body receives large impact load that causes, in some cases, destruction of the primary structure of the rocket. In this paper, we discuss structural design of K-class hybrid rockets with load analysis of parachute opening shock.

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© 2008 The Japan Society of Mechanical Engineers
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