Modern engineering for design of liquid-propellant rocket engines /

Detalles Bibliográficos
Autor Principal: Huzel, Dieter K.
Otros autores o Colaboradores: Huang, David H.
Formato: Libro
Lengua:inglés
Datos de publicación: Washington DC : American Institute of Aeronautics and Astronautics, 1992.
Series:Progress in astronautics and aeronautics ; 147
Temas:
Resumen: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.
Descripción Física:431 p. : il.
ISBN:1563470136
ISSN:00796050