Numerical modeling and parametric analysis of performance of a monopropellant thruster using a single-part catalyst bed model-Reference-Cited by-同舟云学术

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Numerical modeling and parametric analysis of performance of a monopropellant thruster using a single-part catalyst bed model

Published:2023-09-26 Issue:1 Volume:28 Page:36-64
ISSN:1364-7830
Container-title:Combustion Theory and Modelling
language:en
Short-container-title:Combustion Theory and Modelling

Author:

Salimi Mohammad Reza¹,Karimaei Hadiseh¹,Gholampour Yazdi Mostafa¹

Affiliation:

1. Aerospace Research Institute, Ministry of Science, Research and Technology, Tehran, Iran

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,Modeling and Simulation,General Chemical Engineering,General Chemistry

Link

https://www.tandfonline.com/doi/pdf/10.1080/13647830.2023.2258841

Reference40 articles.

1. Kinetics and Mechanism of Thermal and Catalytic Decomposition of Hydroxylammonium Nitrate (HAN) Monopropellant

2. Catalytic bed slenderness ratio and ADN/methanol ratio for decomposition and combustion characteristics within ammonium dinitramide (ADN)-based green aerospace thruster

3. Pore-scale flow and mass transport in gas diffusion layer of proton exchange membrane fuel cell with interdigitated flow fields

4. Pore-scale study of pore-ionomer interfacial reactive transport processes in proton exchange membrane fuel cell catalyst layer

5. Steady State Analysis of Hydrazine Catalytic Thrusters for Different Types of Catalysts

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