Modeling Combustion of Hydrazinium Nitroformate
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference24 articles.
1. Simplified Combustion Modeling of Double Base Propellant: Gas Phase Chain Reaction Vs. Thermal Decomposition
2. Brewster, M. Q., Ward, M. J., and Son, S. F. "New Paradigm for Simplified Combustion Modeling of Energetic Solids: Branched Chain Gas Reaction," AIAA Paper 97-3333, 33r dAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Seattle, WA, July6-9,1997.
3. Schoyer, H. F. R., Korting, P. A. O. G., Veltmans, W. H. M., Louwers, J., v. d. Heijden, A. E. D. M., Keizers, H. L. J., and v. d. Berg, R. P. "An Overview of the Development of HNF and HNFbased Propellants," AIAA Paper 2000-3184, 36thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, AL, July16-19,2000.
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