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Ducted rocket engine

The chemical compositions of the gas-generating propellants for ducted rocket engines are different from those of the propellants used for rocket motors. The physicochemical properties of the gas-generating propellants used for variable flow systems are[12,13]... [Pg.227]

Choking. A common expression for use of the constricted nozzle(, choke ) to control the flow of gas from a rocket engine thrust chamber by building up pressure inside the chamber until the upper limit of mass flow is reached, or when the speed of sound is reached in the duct... [Pg.57]

See other pages where Ducted rocket engine is mentioned: [Pg.103]    [Pg.483]    [Pg.103]    [Pg.483]    [Pg.94]    [Pg.225]    [Pg.225]    [Pg.225]    [Pg.226]    [Pg.226]    [Pg.227]    [Pg.229]    [Pg.103]    [Pg.483]    [Pg.103]    [Pg.483]    [Pg.94]    [Pg.225]    [Pg.225]    [Pg.225]    [Pg.226]    [Pg.226]    [Pg.227]    [Pg.229]    [Pg.488]    [Pg.515]    [Pg.3]    [Pg.527]    [Pg.175]    [Pg.777]    [Pg.205]    [Pg.843]    [Pg.370]   
See also in sourсe #XX -- [ Pg.483 ]

See also in sourсe #XX -- [ Pg.483 ]



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