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.
Full Spectrum Crashworthiness Criteria for Rotorcraft
2011
163 pages
Report
Keine Angabe
Englisch
Aeronautics , Aircraft , Air Transportation , Military Sciences , Crashworthiness , Design criteria , Helicopters , Aeronautical engineering , Protection , Requirements , Standards , Survivability , Systems engineering , Airframe crashworthiness , Conventional rotorcraft , Crash data analysis , Crashworthiness index , Crashworthy designs , Full spectrum criteria , Military rotorcraft , Occupant protection , System design , Tandem rotorcraft , Tilt rotor rotorcraft
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