Modern engineering for design of liquid-propellant rocket engines / Dieter K. Huzel and David H. Huang.
Tipo de material: TextoSeries Progress in astronautics and aeronautics ; 147Detalles de publicación: Washington DC : American Institute of Aeronautics and Astronautics, 1992.Descripción: 431 p. : ilISBN:- 1563470136
Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
---|---|---|---|---|---|
Koha Ingenieria | 629.76 HUZ Bloque 19 (Navegar estantería(Abre debajo)) | Disponible | 35764 |
Introduction to liquid-propellant rocket engines - Engine requirements and preliminary design analyses - Introduction to sample calculations - Design of thrust cambers and other combustion devices - Design of gas-pressurized propellant feed systems - Design of turbopump propellant feed systems - Design of turbopump propellant feed systems - Design of rocket-engine control and condition-monitoring systems - Design of propellant tanks - Design of interconnecting components and mounts - Engine systems design integration - Design of liquid-propellant space engines - Appendices.
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