Numerical Simulation of Ignition Process for the Monomethyl Hydrazine–Nitrogen Tetroxide Thrusters-Reference-Cited by-同舟云学术

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Numerical Simulation of Ignition Process for the Monomethyl Hydrazine–Nitrogen Tetroxide Thrusters

Published:2019-07 Issue:4 Volume:35 Page:704-719
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Wei Qiang¹,Liang Guozhu¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics, 100083 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B37136

Reference31 articles.

1. Supercomputer modeling of hydrogen combustion in rocket engines

2. Vaporization Lengths of Hydrazine Fuels Burning with NTO

3. Development of a fundamental model of hypergolic ignition in space-ambient engines.

4. Modeling Hypergolic Ignition in the Army's Impinging Stream Vortex Engine Including Injection Throttling

5. Investigation of Combustion Instability in Small MMH-NTO Liquid Rocket Engines Using CFD

Cited by 8 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. Theoretical study of the second- and third-H-abstraction reactions of monomethylhydrazine and nitrogen dioxide and its application to hypergolic ignition modeling;Combustion and Flame;2024-10

2. Optimal Liquid Engine Architecture by Performance-Cooling Tradeoff Analysis;Journal of Propulsion and Power;2024-07

3. Computational Modelling of MMH/NTO Combustion in a Multi-element Triplet Injector Combustor;Lecture Notes in Mechanical Engineering;2024

4. AN INTER-IMPINGEMENT SPRAY MODEL CONSIDERING BINARY DROPLET COLLISION BASED ON OPENFOAM;Atomization and Sprays;2024

5. Thermal performance of MMH/NTO rocket thrust chamber based on pintle injector by using liquid film cooling;Applied Thermal Engineering;2023-03

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