Implementation study of a passive safety feature in the rescue systems of small aircrafts
Abstract
The aim of this paper is to evaluate the feasibility of implementation of a passive safety feature in the form of an under-fuselage airbag in the rescue systems of small aircraft. The paper presents a multidisciplinary approach for the viability of the implementation. It presents the development of mathematical model for airbag performance analysis. The model is validated against the experimental data to account for various simplifications. Validated mathematical model is used to design a full-scale airbag for the chosen airplane to perform in the designed range. Weight penalty for increased safety is determined.
Keyword : parachute rescue, passive safety, airbag, impact attenuation, experimental validation, ultralight aircraft
This work is licensed under a Creative Commons Attribution 4.0 International License.
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