Internal ballistics of solid-fuel rockets : Military rockets using dry-processed. double-base propellant as fuel
Tipo de material:
TextoDetalles de publicación: New York : McGraw-Hill, 1950.Descripción: 214 pTema(s):
Contenidos:
Relation of internal to external ballistics - Characteristics of propellant gases - Burning properties of propellants - Steady-state flow of compressible fluids - Nozzle performance - Flow of gas inside rocket motors - Determination of reaction pressures in rocket motors - Design of propellant grains - Characteristics of burning in perforations - Ignition - Effect of physical properties of propellant on ballistic performance - End-burning grains - Static testing equipment - Heat transfer
Libro
| Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
|---|---|---|---|---|---|
| Koha Ingenieria | 629.76 WIM Bloque 19 (Navegar estantería(Abre debajo)) | Disponible | 32865 |
Relation of internal to external ballistics - Characteristics of propellant gases - Burning properties of propellants - Steady-state flow of compressible fluids - Nozzle performance - Flow of gas inside rocket motors - Determination of reaction pressures in rocket motors - Design of propellant grains - Characteristics of burning in perforations - Ignition - Effect of physical properties of propellant on ballistic performance - End-burning grains - Static testing equipment - Heat transfer
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