Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition
- 1 January 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 20 (1), 87-92
- https://doi.org/10.2514/1.9234
Abstract
No abstract availableKeywords
This publication has 25 references indexed in Scilit:
- Propellant Technologies: Far-Reaching Benefits for Aeronautical and Space-Vehicle PropulsionJournal of Propulsion and Power, 1998
- Nontoxic Orbital Maneuvering and Reaction Control Systems for Reusable SpacecraftJournal of Propulsion and Power, 1998
- Status and Issues Related to In-Space Propulsion SystemsJournal of Propulsion and Power, 1998
- A Laser DiagnosticTechnique to Measure Chemical DelayTime in Hypergolic CombustionCombustion Science and Technology, 1998
- Rate constant for the NH3 + NO2 ? NH2 + HONO reaction: Comparison of kinetically modeled and predicted resultsInternational Journal of Chemical Kinetics, 1997
- Temperature profile and ignition delay studies on hypergolic systemsCombustion and Flame, 1990
- Atmospheric chemistry of propellant vaporsToxicology Letters, 1989
- Chemical aspects of the hypergolic preignition reactions of some hybrid hypergolsCombustion and Flame, 1987
- Reaction between ammonia and nitrogen dioxideJournal of the Chemical Society, Faraday Transactions 1: Physical Chemistry in Condensed Phases, 1972
- Development of a fundamental model of hypergolic ignition in space-ambient engines.AIAA Journal, 1967