Aerotecnica Missili & Spazio
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Evaluation of the Biomechanical Responses During an Aircraft Emergency Landing
Aerotecnica Missili & Spazio - Tập 101 - Trang 121-133 - 2022
Passengers’ safety in unconventional situations, such as those of an emergency
landing, has become more and more important due to the increase of air traffic.
To improve passengers’ safety, certification authorities have imposed specific
crashworthiness requirements in airworthiness regulations as defined in Title 14
of Federal Regulations Code—Part 25 for transport aircraft. Over the years, a
ser...
Non-linear modelling for Multi-Disciplinary and Multi-Objective Optimization of a complete aircraft
Aerotecnica Missili & Spazio - Tập 92 Số 1-2 - Trang 61-68 - 2013
Reliability Centered Maintenance Analysis Using Analytic Hierarchy Process for Electro-mechanical Actuators
Aerotecnica Missili & Spazio - Tập 100 - Trang 321-335 - 2021
There is an increasing trend for the usage of electrically powered equipment in
the aviation industry. In this paper, a Reliability Centered Maintenance (RCM)
analysis application is performed for Electro-Mechanical Actuators (EMA). We
consider a new model for criticality classification for individual failure modes
for the Reliability Centered Maintenance analysis stages using the Analytic
Hierarc...
Occupants’ Injury during a Drop Test of an Advanced Composite Fuselage Section
Aerotecnica Missili & Spazio - Tập 97 - Trang 129-134 - 2018
The emergency landing is an important design criteria in airworthiness
certification. It is associated to the cabin safety and consequently to the risk
of serious injury for the occupant. The loads transmitted to the passengers
during a hard landing can be fatal both in terms of intensity and duration time,
and the energy absorbing systems play a fundamental role to dissipate the
energies unleashe...
Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines
Aerotecnica Missili & Spazio - - 2022
AbstractThe low regression rate of Hybrid Rocket Engines (HREs) is one prominent
characteristic that is addressed in most abstracts concerning hybrid propulsion.
Over the years, researchers developed and investigated numerous ways to tackle
the low regression rate problem of HREs. This article is a collection and
assessment of these diverse methods and designs. It allows for a quick overview
of th...
A global exploration method to identify families of cycling Earth–Mars trajectories
Aerotecnica Missili & Spazio - Tập 99 Số 3 - Trang 187-194 - 2020
Determining Dynamic Stability of a Re-entry Capsule at Free Fall
Aerotecnica Missili & Spazio - - Trang 1-16 - 2023
Re-entry capsules, designed with blunt-body shapes to endure hypersonic air
velocities and heat, encounter instability in the low subsonic regime during the
final descent phase. Ensuring a controlled descent with the appropriate attitude
for deploying deceleration systems becomes paramount. To address this challenge,
we employ a cost-effective approach to investigate the dynamic stability of a
typ...
Tổng số: 223
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