Materials for Missiles and Spacecraft / John C. McDonald...[et al.]
Tipo de material:
Contenidos:
General criteria for the design and manufacture of missiles and spacecraft - Materials at cryogenic temperatures - Extreme high temperature materials - Materials for thermal protection - Compatibility of materials - Choice of materials and fabrication technoques for pressure vessels - Fracture of pressure vessels -Temperature control of spacecraft - Evaporation effects on materials in space - Lubrication - Nuclear materials and problems - Materials for direct conversion - The economic aspects of materials and their applications in missiles and spacecraft

Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
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Koha Ingenieria | 629.76 PAR -Bloque 19 (Navegar estantería(Abre debajo)) | Disponible | A2193 |
Navegando Koha Ingenieria estanterías Cerrar el navegador de estanterías (Oculta el navegador de estanterías)
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629.76 FLO- Bloque 19 Réacteurs-fusées | 629.76 HUZ Bloque 19 Modern engineering for design of liquid-propellant rocket engines / | 629.76 MCG-Bloque 19 Astronautics | 629.76 PAR -Bloque 19 Materials for Missiles and Spacecraft / | 629.76 PRI I-Bloque 19 Space Flight 1 : Environment and Celestial Mechanics | 629.76 PRI II-Bloque 19 Space Flight II : Dynamics | 629.76 ROS-Bloque 19 Mathematical theory of rocket flight. |
General criteria for the design and manufacture of missiles and spacecraft - Materials at cryogenic temperatures - Extreme high temperature materials - Materials for thermal protection - Compatibility of materials - Choice of materials and fabrication technoques for pressure vessels - Fracture of pressure vessels -Temperature control of spacecraft - Evaporation effects on materials in space - Lubrication - Nuclear materials and problems - Materials for direct conversion - The economic aspects of materials and their applications in missiles and spacecraft
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