Numerical simulation for the decomposition of DT-3 in a monopropellant thruster-Reference-Cited by-同舟云学术

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Numerical simulation for the decomposition of DT-3 in a monopropellant thruster

Published:2018-03 Issue: Volume:74 Page:132-144
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Gao Zi-guang,Li Guo-xiu,Zhang Tao,Liu Xu-hui,Wang Zi-huan,Liu Xin

Funder

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Kinetic modeling of the decomposition and flames of hydrazine;Konnov;Combust. Flame,2001

2. Study on Catalytic Decomposition of DT-3;Zhao,2002

3. Toxic effects of rocket propellant DT-3 on lung tissues of rats;Zhang;Asian J. Ecotoxicol.,2008

4. Liquid Propellant;Li,2011

5. Design and research on catalyst bed of hydrazine–hydrazine nitrate-water engine;Zhou;Aerosp. Shanghai,1994

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1. A DFT investigation of hydrazine nitrate dissociation mechanism on MoN(0 0 1);Computational and Theoretical Chemistry;2024-05

2. Effects of ignition voltage and electrode structure on electric ignition and combustion characteristics of Ammonium Dinitramide (ADN)-based liquid propellants in electric ignition mode in inert gas environment;Chinese Journal of Aeronautics;2024-04

3. Numerical modeling and parametric analysis of performance of a monopropellant thruster using a single-part catalyst bed model;Combustion Theory and Modelling;2023-09-26

4. A Dft Investigation of Hydrazine Nitrate Dissociation Mechanism on Mon(001);2023

5. DFT study on decomposition of hydrazine nitrate on Ir(1 0 0) surface;Computational and Theoretical Chemistry;2022-11

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