Ignition of hypergolic propellants in a simulated space environment.
Author:
Affiliation:
1. Celestial Research Corporation, South Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28852
Reference8 articles.
1. Flammability Characteristics of Hydrazine Fuels in Nitrogen Tetroxide Atmospheres.
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3. Kinetics Modeling of Hypergolic Propellants;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12
4. 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
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