Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition-Reference-Cited by-同舟云学术

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Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition

Published:2004-01 Issue:1 Volume:20 Page:87-92
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Catoire Laurent¹,Chaumeix Nabiha¹,Paillard Claude¹

Affiliation:

1. Centre National de la Recherche Scientifique and University of Orleans, F-45071 Orleans CEDEX 02, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.9234

Reference30 articles.

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

2. A Laser DiagnosticTechnique to Measure Chemical DelayTime in Hypergolic Combustion

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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

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3. Insights into the Reaction Kinetics of Hydrazine-Based Fuels: A Comprehensive Review of Theoretical and Experimental Methods;Energies;2023-08-16

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

5. An Unsteady Hypergolic Combustion Modeling Tool Based on Compressible Three-Stream Flamelet Methodology;AIAA SCITECH 2023 Forum;2023-01-19

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