LOX/methane reusable rocket propulsion at reach with large scale demonstrators tested-Reference-Cited by-同舟云学术

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LOX/methane reusable rocket propulsion at reach with large scale demonstrators tested

Published:2018-11 Issue: Volume:152 Page:542-556
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Boué Yoan,Vinet Pierre,Magniant Sonia,Motomura Taiichi,Blasi Roland,Dutheil Jean-Philippe

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference7 articles.

1. Characterisation of a LOX/LCH4 gas generator;Soller,2014

2. Airbus defence and Space LOX/methane propulsion demonstrator;Magniant S,2014

3. 2MW LOX/Methane turbopump demonstrator reusable and designed-to-safety passed through test;Magniant,2016

4. LOX/Methane thrust chamber demonstrator testing;Blasi,2016

5. LOX/Methane thrust chamber demonstrator- from subscale to full scale testing;Blasi,2016

Cited by 21 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A system-level multi-field coupling algorithm for regenerative cooling thrust chamber of a LOX/methane rocket engine;Acta Astronautica;2023-12

2. Numerical Investigation of Turbopump Bearing Heat Generation in Liquid Methane;Journal of Tribology;2023-05-02

3. Numerical study of combustion and cooling performance of a gaseous oxygen and gaseous methane rocket combustor with the needle-bolt injector;Applied Thermal Engineering;2023-02

4. Performance Characteristics of the Film-cooling System Applied to 200 N-class GCH₄-LOx Small Rocket Engine;AIAA SCITECH 2023 Forum;2023-01-19

5. RANS based numerical simulation of a GCH4/GO2 rocket engine combustion chamber with film cooling and improvement of wall heat flux prediction;Applied Thermal Engineering;2023-01

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