Experimental investigation of the effect of nozzle throat diameter on the performance of a hybrid rocket motor with swirling injection of high-concentration hydrogen peroxide-Reference-Cited by-同舟云学术

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Experimental investigation of the effect of nozzle throat diameter on the performance of a hybrid rocket motor with swirling injection of high-concentration hydrogen peroxide

Published:2019-11 Issue: Volume:164 Page:334-344
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wei S.S.,Lee M.C.,Chien Y.H.,Chou T.H.,Wu J.S.

Funder

National Chiao Tung University

Ministry of Science and Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Nano/Microsatellite Market Forecast;Doncaster,2017

2. Autoignitable and restartable hybrid rockets using catalytic decomposition of an oxidizer;Jung;J. Propuls. Power,2014

3. Experimental tests of throttleable H2O2/PE hybrid rocket motors;Zhao,2015

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