Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor

Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor

Effects of swirling oxidizer flow on the performance of a HTPB/N2O Hybrid rocket motor were studied. A hybrid propulsion laboratory has been developed, to characterize internal ballistics characteristics of swirl flow hybrid motors and to define the operating parameters, like fuel regression rate, s...

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Bibliographic Details
Main Authors:	Mohammad Mahdi Heydari, Nooredin Ghadiri Massoom
Format:	Article
Language:	English
Published:	Hindawi Limited 2017-01-01
Series:	International Journal of Aerospace Engineering
Online Access:	http://dx.doi.org/10.1155/2017/3174140

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