Parametric study and performance analysis of hybrid rocket motors with double-tube configuration-Reference-Cited by-同舟云学术

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Parametric study and performance analysis of hybrid rocket motors with double-tube configuration

Published:2017-03 Issue: Volume:132 Page:90-96
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yu Nanjia,Zhao Bo,Lorente Arnau Pons,Wang Jue

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. Gaseous oxygen injection effects in hybrid Labscale Rocket;Gomes S.R;Mot. Oper. AIAA Pap.,2010

2. Study on hybrid rocket with;Ohe;AIAA Pap.,2014

3. Performance and analysis of vortex oxidizer injection in a hybrid rocket motor;Jones;AIAA Pap.,2009

4. Development and three-dimensional numerical simulation of a double-tube hybrid rocket motor;Pons Lorente;AIAA Pap.,2014

5. Testing and evaluation of a double-tube hybrid rocket;Pons Lorente;Mot., AIAA Pap.,2015

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1. Performance estimation of hybrid rocket by varying the flow rate at multi-location swirl injector;FirePhysChem;2024-08

2. Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines;Aerotecnica Missili & Spazio;2022-05-24

3. Review on the regression rate-improvement techniques and mechanical performance of hybrid rocket fuels;FirePhysChem;2021-12

4. Transient investigation of nozzle erosion in a long-time working hybrid rocket motor;Aerospace Science and Technology;2021-11

5. Effect of multi-location swirl injection on the performance of hybrid rocket motor;Acta Astronautica;2020-11

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