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Aerospace Engineering on the Back of an Envelope [electronic resource] / by Irwin E. Alber.

Por: Tipo de material: TextoTextoSeries Springer Praxis Books | Springer Praxis BooksEditor: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer, 2012Descripción: XXII, 326 p. online resourceTipo de contenido:
  • text
Tipo de medio:
  • computer
Tipo de soporte:
  • online resource
ISBN:
  • 9783642225376
Trabajos contenidos:
  • SpringerLink (Online service)
Tema(s): Formatos físicos adicionales: Sin títuloClasificación CDD:
  • 629.1 23
Clasificación LoC:
  • TL787-4050.22
Recursos en línea:
Contenidos:
Springer eBooksResumen: Engineers need to acquire ǣBack-of-the-Envelopeǥ survival skills to obtain rough quantitative answers to real-world problems, particularly when working on projects with enormous complexity and very limited resources. In the case studies treated in this book, we show step-by-step examples of the physical arguments and the resulting calculations obtained using the quick-fire method. We also demonstrate the estimation improvements that can be obtained through the use of more detailed physics-based Back-of-the-Envelope engineering models. These different methods are used to obtain the solutions to a number of design and performance estimation problems arising from two of the most complex real-world engineering projects: the Space Shuttle and the Hubble Space Telescope satellite.
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Space Shuttle Performance Estimates -- Columbia Shuttle Accident Analysis -- Reentry and Landing of the Orbiter -- Hubble Space Telescope Design -- Solenoid Robot Kicker Design using BotE Techniques.

Engineers need to acquire ǣBack-of-the-Envelopeǥ survival skills to obtain rough quantitative answers to real-world problems, particularly when working on projects with enormous complexity and very limited resources. In the case studies treated in this book, we show step-by-step examples of the physical arguments and the resulting calculations obtained using the quick-fire method. We also demonstrate the estimation improvements that can be obtained through the use of more detailed physics-based Back-of-the-Envelope engineering models. These different methods are used to obtain the solutions to a number of design and performance estimation problems arising from two of the most complex real-world engineering projects: the Space Shuttle and the Hubble Space Telescope satellite.

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