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Calculated Condenser Performance for a Mercury-Turbine Power Plant for Aircraft by Ronald B. Doyle, Nasa Technical Reports Server (Ntrs) - Paperback
58.80 AED

Calculated Condenser Performance for a Mercury-Turbine Power Plant for Aircraft by Ronald B. Doyle, Nasa Technical Reports Server (Ntrs) - Paperback

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Category Type
Politics
ISBN
9781287264637
Author
Ronald B. Doyle, Nasa Technical Reports Server (Ntrs)
Publisher
Bibliogov
Description:

As part of an investigation af the application of nuclear energy to various types of power plants for aircraft, calculations have been made to determine the effect of several operating conditions on the performance of condensers for mercury-turbine power plants. The analysis covered 8 range of turbine-outlet pressures from 1 to 200 pounds per square inch absolute, turbine-inlet pressures ...

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    Specifications

    Category Type
    Politics
    ISBN
    9781287264637
    Item EAN
    2724352844607
    People
    Author
    Ronald B. Doyle, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Category Type
    Politics
    ISBN
    9781287264637
    Item EAN
    2724352844607
    People
    Author
    Ronald B. Doyle, Nasa Technical Reports Server (Ntrs)
    People
    Publisher
    Bibliogov
    Technical Information
    Binding
    Paperback
    Languages and countries
    Book Language
    English
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  •  

    Description:

    As part of an investigation af the application of nuclear energy to various types of power plants for aircraft, calculations have been made to determine the effect of several operating conditions on the performance of condensers for mercury-turbine power plants. The analysis covered 8 range of

    As part of an investigation af the application of nuclear energy to various types of power plants for aircraft, calculations have been made to determine the effect of several operating conditions on the performance of condensers for mercury-turbine power plants. The analysis covered 8 range of turbine-outlet pressures from 1 to 200 pounds per square inch absolute, turbine-inlet pressures from 300 to 700 pounds per square inch absolute, and a range of condenser cooling-air pressure drops, airplane flight speeds, and altitudes. The maximum load-carrying capacity (available for the nuclear reactor, working fluid, and cargo) of a mercury-turbine powered aircraft would be about half the gross weight of the airplane at a flight speed of 509 miles per hour and an altitude of 30,000 feet. This maximum is obtained with specific condenser frontal areas of 0.0063 square foot per net thrust horsepower with the condenser in a nacelle and 0.0060 square foot per net thrust horsepower with the condenser submerged in the wings (no external condenser drag) for a turbine-inlet pressure of 500 pounds per square inch absolute, a turbine-outlet pressure of 10 pounds per square inch absolute, and 8 turbine-inlet temperature of 1600 F.

    Product Features:
    • Category: Politics
    • Binding: Paperback
    • Language of Text: English
    • Author(s): Ronald B. Doyle, Nasa Technical Reports Server (Ntrs)
    • Publisher: Bibliogov
    • ISBN: 9781287264637
    • Number of Pages: 26
    • Dimensions: 9.69 x 7.44 x 0.05 inches
 

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