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Liquid ramjet

Solid Rockets, Liquid Ramjets, and Ducted Rockets... [Pg.439]

Ducted rockets are intermediate between solid rockets and liquid ramjets in their propulsion characteristics. The propulsive force of soHd rockets is generated by the combustion of propellants composed of oxidizer and fuel components. Thus, no additional fuels or oxidizers need to be introduced from the atmosphere into the rocket motor. The momentum change of the exhaust gas from the nozzle attached to the aft-end of the combustion chamber is converted into the thrust for propulsion. On the other hand, the propulsive force of Hquid ramjets is generated by the combustion of a liquid hydrocarbon fuel with air introduced from the atmo-sphere.Ii] jjjg incoming air is compressed by a shock wave formed at the air-intake attached to the front end of the combustor. The air taken in from the atmosphere serves only as the oxidizer for the ramjets. The thrust is created by the momentum difference between the exhaust gas from the combustor and the air taken in from the atmosphere. [Pg.439]

LIQUID-FUELED ACTIVE CONTROL FOR RAMJET COMBUSTORS... [Pg.333]

Model ramjet dump combustor with direct liquid-fuel injection for... [Pg.341]

See other pages where Liquid ramjet is mentioned: [Pg.225]    [Pg.225]    [Pg.10]    [Pg.333]    [Pg.488]    [Pg.439]    [Pg.526]    [Pg.592]    [Pg.439]    [Pg.37]    [Pg.360]    [Pg.515]    [Pg.526]    [Pg.592]    [Pg.81]    [Pg.175]    [Pg.169]    [Pg.274]    [Pg.657]    [Pg.121]    [Pg.129]   
See also in sourсe #XX -- [ Pg.439 ]

See also in sourсe #XX -- [ Pg.439 ]



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