Flame structure of GCH4/GOX pintle model combustor with wall confinement-Reference-Cited by-同舟云学术

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Flame structure of GCH4/GOX pintle model combustor with wall confinement

Published:2024-02 Issue: Volume:145 Page:108842
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kim Dae Hwan,Jo Hyeontaek,Heo Subeom,Yoon Youngbin

Funder

Ministry of Science, ICT and Future Planning

National Research Foundation of Korea

Korea Institute of Energy Technology Evaluation and Planning

Institute of Advanced Aerospace Technology, Seoul National University

Seoul National University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. Summary of deep throttling rocket engines with emphasis on apollo LMDE, AIAA, 5220;Dressler,2006

2. Liquid-propellant rocket engine throttling: a comprehensive review;Casiano;J. Propul. Power,2010

3. Summarization on variable liquid thrust rocket engines;Yue;Sci. China Ser. E Technol. Sci.,2009

4. Guidance summary and assessment of the Chang'e-3 powered descent and landing;Li;J. Spacecr. Rockets,2016

5. Development trends of reusable launch vehicles;Yun;KSPE,2023

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