A study of both landbased and shipboard tests of the F14A aircraft with the MK7 Jet Blast Deflector to investigate the effect of backflow of jet exhaust on the aircraft being launched and the resulting environmental temperature aft and alongside the JBD. Configuration for shipboard installation and desired mode of operation are recommended. Areas for further effort to achieve improved compatibility are also presented. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Environmental Temperature and Aircraft Compatibility Studies


    Contributors:
    G. Gaeman (author) / W. Goon (author)

    Publication date :

    1972


    Size :

    77 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Environmental Compatibility of CRYOPLANE the Cryogenic-fuel Aircraft

    Klug, H. / France; Office national d'etudes et de recherches aerospatiales | British Library Conference Proceedings | 1996


    Aircraft electromagnetic compatibility

    Clarke, Clifton A. / Larsen, William E. | NTRS | 1987