The technology of thermionic thermal protection of thermostressed elements for aviation and space equipment is discussed. This technology is based on the thermionic emission phenomenon. Estimations of temperature decrease of the surface of thermostressed subsystems of reusable spacecraft and orbital launch vehicles at the thermionic thermal protection application are given.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 62 , 4 ; 669-674


    Publication date :

    2019-10-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles

    Kolychev, A. V. / Kernozhitskii, V. A. / Chernyshov, M. V. | Online Contents | 2019


    Reusable launch vehicles

    DrDr Ruppe, H.O. | Elsevier | 1985


    Reusable launch vehicles

    Osmun, W.G. | Engineering Index Backfile | 1964



    Reusable Space Launch Vehicles

    Hammond, Walter | AIAA | 1999