Alexander shteinberg (32 risultati)
Fast Reactions in Energetic Materials. High-Temperature Decomposition of Rocket Propellants and Explosives
Shteinberg, Alexander S. Translated from Russian by Maria Rusanova
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Production of Advanced Materials by Methods of Self-Propagating High-Temperature Synthesis
Tavadze, Giorgi F.; Shteinberg, Alexander S.; Rusanova, Maria (TRN)
Lingua: Inglese
Editore: Springer 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Production of Advanced Materials by Methods of Self-Propagating High-Temperature Synthesis
Tavadze, Giorgi F.; Shteinberg, Alexander S.; Rusanova, Maria (TRN)
Lingua: Inglese
Editore: Springer 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Production of Advanced Materials by Methods of Self-Propagating High-Temperature Synthesis
Tavadze, Giorgi F.; Shteinberg, Alexander S.; Rusanova, Maria (TRN)
Lingua: Inglese
Editore: Springer 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Production of Advanced Materials by Methods of Self-Propagating High-Temperature Synthesis
Tavadze, Giorgi F.; Shteinberg, Alexander S.; Rusanova, Maria (TRN)
Lingua: Inglese
Editore: Springer 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Lingua: Inglese
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Paperback. Condizione: Brand New. translation edition. 156 pages. 9.00x6.25x0.50 inches. In Stock.
Lingua: Inglese
Editore: Springer Berlin Heidelberg 2013
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Taschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - This translation from the original Russian book outlines the production of a variety of materials by methods of self-propagating high-temperature synthesis (SHS). The types of materials discussed include: hard, refractory, corrosion and wear-resis…tant materials, as well as other advanced and speciality materials. The authors address the issue of optimal parameters for SHS reactions occurring during processes involving a preliminary metallothermic reduction stage, and they calculate this using thermodynamic approaches. In order to confirm the effectiveness of this approach, the authors describe experiments focussing on the synthesis of elemental crysalline boron, boron carbides and nitrides. Other parts of this brief include theoretical and experimental results on single-stage production of hard alloys on the basis of titanium and zirconium borides, as well as macrokinetics of degassing and compaciton of SHS-products.This brief is suitable for academics, as well as those working in industrial manufacturing companies producing hard alloys and composites for making metal-working machinery or drilling equipment.
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Condizione: New. pp. 216.
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Taschenbuch. Condizione: Neu. Fast Reactions in Energetic Materials | High-Temperature Decomposition of Rocket Propellants and Explosives | Alexander S. Shteinberg | Taschenbuch | xiv | Englisch | 2010 | Springer | EAN 9783642097676 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, j…uergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.
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Taschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hybrid) is…currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Berlin Heidelberg 2008
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Buch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hybrid) is current…ly of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.
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Ensayo. Ciencia. Física. Química. Idiomas-Inglés.Germany. Editorial: Springer. 2006. No indica edición. 201 pags. 24x16 cms. Cartoné editorial. Muy buen estado. GASTOS DE ENVÍO: 1 EURO PARA EL ENVÍO ORDINARIO (SIN NÚMERO DE SEGUIMIENTO). 2,50 EUROS PARA EL ENVÍO CERTIFICADO CON RECOGIDA EN OFICINA DE CORREOS. 3,50 EUROS PARA EL…ENVÍO CERTIFICADO CON ENTREGA EN DOMICILIO.
Lingua: Inglese
Editore: Springer Berlin Heidelberg Jan 2013 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This translation from the original Russian book outlines the production of a variety of materials by methods of self-propagating high-temperature synthesis (SHS). The types of materials discussed include: hard, refractory, corrosio…n and wear-resistant materials, as well as other advanced and speciality materials. The authors address the issue of optimal parameters for SHS reactions occurring during processes involving a preliminary metallothermic reduction stage, and they calculate this using thermodynamic approaches. In order to confirm the effectiveness of this approach, the authors describe experiments focussing on the synthesis of elemental crysalline boron, boron carbides and nitrides. Other parts of this brief include theoretical and experimental results on single-stage production of hard alloys on the basis of titanium and zirconium borides, as well as macrokinetics of degassing and compaciton of SHS-products.This brief is suitable for academics, as well as those working in industrial manufacturing companies producing hard alloys and composites for making metal-working machinery or drilling equipment. 176 pp. Englisch.
Lingua: Inglese
Editore: Springer Berlin Heidelberg 2013
Serie: SpringerBriefs in Materials, Libro 3 di 68. Libro 3 di 68 - SpringerBriefs in Materials
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Kartoniert / Broschiert. Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Outlines the production of a unique composite material (Ti - TiB) Describes a new method of synthesis of elemental boron and refractory boridesThis translation from the original Russian book…outlines the production of a variety of material.
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Buch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hy…brid) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels. 216 pp. Englisch.
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Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid… and hybrid) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels. 216 pp. Englisch.
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. The major part of the experimental results presented in the book has not been published beforeFor the first time these studies are available in EnglishCombining theoretical and experimental parts including a descript…ion of novel methodologi.
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. The major part of the experimental results presented in the book has not been published beforeFor the first time these studies are available in EnglishCombining theoretical and experimental parts including a descript…ion of novel methodologi.
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Buch. Condizione: Neu. Fast Reactions in Energetic Materials | High-Temperature Decomposition of Rocket Propellants and Explosives | Alexander S. Shteinberg | Buch | xiv | Englisch | 2008 | Springer-Verlag GmbH | EAN 9783540788607 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, jue…rgen[dot]hartmann[at]springer[dot]com | Anbieter: preigu Print on Demand.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Berlin Heidelberg Sep 2008 2008
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Buch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and hybrid…) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 216 pp. Englisch.
Lingua: Inglese
Editore: Springer Berlin Heidelberg, Springer Okt 2010 2010
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Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Modern energetic materials include explosives, blasting powders, pyrotechnic m- tures and rocket propellants [1, 2]. The study of high-temperature decomposition of condensed phases of propellants and their components (liquid, solid and… hybrid) is currently of special importance for the development of space-system engineering [3, 4]. To better understand the burning mechanisms (stationary, nonstationary, - steady) of composite solid propellants and their components, information about the macrokinetics of their high-temperature decomposition is required [5]. To be able to evaluate the ignition parameters and conditions of safe handling of heat-affected explosives, one needs to know the kinetic constants of their high-temperature - composition. The development of new composite solid propellants characterized by high performance characteristics (high burning rates, high thermal stability, stability to intrachamber perturbations, and other aspects) is not possible without quanti- tive data on the high-temperature decomposition of composite solid propellants and their components [6]. The same reasons have resulted in signi cant theoretical and practical interest in the high-temperature decomposition of components of hybrid propellants. It is known that hybrid propellants have not been used very widely due to the low bu- ing (pyrolysis) rates of the polymer blocks in the combustion chambers of hybrid rocket engines. To increase the burning rates it is necessary to obtain information about their relationships to the corresponding kinetic and thermophysical prop- ties of the fuels.Springer-Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 216 pp. Englisch.
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Condizione: New. Print on Demand pp. 216 49:B&W 6.14 x 9.21 in or 234 x 156 mm (Royal 8vo) Perfect Bound on White w/Gloss Lam.
