The purpose of this document is to establish full-spectrum crashworthiness criteria for implementation starting in the initial stages of system design for a wide range of rotorcraft classes, types, configurations, and operating conditions that continue over the life cycle of the rotorcraft system. These criteria will identify the key components that contribute to a system's crashworthiness and will provide a quantitative measure of crashworthy performance that is relevant to user needs and future operating environments.


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    Rotorcraft Full Spectrum Crashworthiness and Occupant Injury Requirements

    Crocco, J. / Jackson, K. / Pellettiere, J. et al. | British Library Conference Proceedings | 2011




    Rotorcraft subfloor design for enhanced crashworthiness characteristics

    Hajela, P. / Lee, E. | British Library Conference Proceedings | 1997