Avionics and electronics for military application must exist in a variety of extreme environments. The Avionics Integrity Program and MIL-STD 810D require the avionics designer to identify the significant environments in the initial phase of the design process, design to exist in the environment, and test to prove reliable operation in the environments. There are two classifications of environments: natural and induced. Natural environments consist of all the environments caused by climatic fluctuations. Induced environments, i.e. vibration and aerodynamic induced heating, are caused by the platform's (vehicle equipment is placed on) interaction with the natural environment. The natural environment is well defined for most deployment locations, but the induced environment varies for each application. Methods for developing induced environmental criteria for vibration and tests are presented.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Vibration Design Criteria for Avionics


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1987



    Publication date :

    1987-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Vibration design criteria for avionics

    LaBrosse Lindsley, M. | Tema Archive | 1987


    Specification Reform of Avionics Thermal Design Criteria - An F-15 Case Study

    Eason, M. / Lutter, R. N. / Smith, T. C. et al. | British Library Conference Proceedings | 2001


    Specification Reform of Avionics Thermal Design Criteria – An F-15 Case Study

    Eason, Myron / Lutter, Robert N. / Smith, Thomas C. | SAE Technical Papers | 2001



    Aircraft Avionics (Digital Avionics Study)

    B. E. Bright / B. List / W. Sen et al. | NTIS | 1973