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Analysis of ETC or Classical Manometric closed vessel tests with coupling of thermodynamic equilibrium calculations: combustion rate, Energy losses Jean Mary Lombard, Barbara Bashung, D. Gr¨ une, A. Carriere, Pascal Andr´ e To cite this version: Jean Mary Lombard, Barbara Bashung, D. Gr¨ une, A. Carriere, Pascal Andr´ e. Analysis of ETC or Classical Manometric closed vessel tests with coupling of thermodynamic equilibrium calculations: combustion rate, Energy losses. 19th International Symposium of Ballistics, 2001, Interlaken, Switzerland. pp.171-178, 2001. <hal-00019659> HAL Id: hal-00019659 https://hal.archives-ouvertes.fr/hal-00019659 Submitted on 1 Mar 2006 HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers. L’archive ouverte pluridisciplinaire HAL, est destin´ ee au d´ epˆ ot et ` a la diffusion de documents scientifiques de niveau recherche, publi´ es ou non, ´ emanant des ´ etablissements d’enseignement et de recherche fran¸cais ou ´ etrangers, des laboratoires publics ou priv´ es.
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Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD

Oct 18, 2020

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Page 1: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD

Analysis of ETC or Classical Manometric closed vessel

tests with coupling of thermodynamic equilibrium

calculations: combustion rate, Energy losses

Jean Mary Lombard, Barbara Bashung, D. Grune, A. Carriere, Pascal Andre

To cite this version:

Jean Mary Lombard, Barbara Bashung, D. Grune, A. Carriere, Pascal Andre. Analysis ofETC or Classical Manometric closed vessel tests with coupling of thermodynamic equilibriumcalculations: combustion rate, Energy losses. 19th International Symposium of Ballistics, 2001,Interlaken, Switzerland. pp.171-178, 2001. <hal-00019659>

HAL Id: hal-00019659

https://hal.archives-ouvertes.fr/hal-00019659

Submitted on 1 Mar 2006

HAL is a multi-disciplinary open accessarchive for the deposit and dissemination of sci-entific research documents, whether they are pub-lished or not. The documents may come fromteaching and research institutions in France orabroad, or from public or private research centers.

L’archive ouverte pluridisciplinaire HAL, estdestinee au depot et a la diffusion de documentsscientifiques de niveau recherche, publies ou non,emanant des etablissements d’enseignement et derecherche francais ou etrangers, des laboratoirespublics ou prives.

Page 2: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD

Page 3: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 4: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 5: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 6: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 7: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 8: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD
Page 9: Analysis of ETC or Classical Manometric closed vessel ... · Figure l, shows the combustion rate of a double base propellant at loading densities of 150 (LD 0.15) and 300 kg/m3 (LD