The work which has been accomplished under this program is reported in two volumes. Volume 1 discusses (1) icing severity level analysis and recommended design criteria, (2) adverse weather protection technology, (3) a trade-off comparison of different types of ice protection systems for various categories of helicopters, and (4) a technology development program for an advanced electrothermal deicing system. Volume 2, Ice Protection System Application to the UH-1H Helicopter, describes the application of the recommended electrothermal deicing system to a UH-1H test aircraft. It provedes a detailed description of the modifications to the basic aircraft (including the flight test-instrumentation) and the results of the ground and flight test program for that aircraft conducted in the winter of 1975-75.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The Development of an Advanced Anti-Icing/Deicing Capability for U.S. Army Helicopters. Volume 1. Design Criteria and Technology Considerations


    Contributors:

    Publication date :

    1975


    Size :

    253 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Environmental Considerations Concerning Anti-Icing / Deicing Agent Application

    Suzuki, S. / Kubo, R. / Yoshie, S. et al. | British Library Conference Proceedings | 2003


    Environmental Considerations Concerning Anti-Icing / Deicing Agent Application

    Suzuki, S. / Kubo, R. / Yoshie, S. et al. | British Library Conference Proceedings | 2003


    Deicing-Anti-Icing Equipment

    Online Contents | 1994


    Aircraft anti-icing and deicing device and anti-icing and deicing method

    CHEN LI / WEN XIN / WANG MINGHUA et al. | European Patent Office | 2023

    Free access