REACTION OF HYDRAZINE AND NITROGEN TETROXIDE IN A LOWPRESSURE ENVIRONMENT
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1956
Reference1 articles.
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1. Insights into the Reaction Kinetics of Hydrazine-Based Fuels: A Comprehensive Review of Theoretical and Experimental Methods;Energies;2023-08-16
2. Chemical Kinetics of Hypergolic Ignition in N2H4/N2O4-NO2 Gas Mixtures;Journal of Propulsion and Power;2014-05
3. Chemical Kinetics of Hypergolic Ignition in Hydrazine/Nitrogen-dioxide Gas Mixtures;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
4. MMH/NTO injection and ignition in vacuum downstream from an Aestus engine single injection element;Aerospace Science and Technology;2004-04
5. Special Project: Fire, Explosion, Compatibility, and Safety Hazards of Nitrogen Tetroxide (AIAA SP-086-2001);2001-01
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