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In an experiment conducted during a Mars mission, a rover propels a projectile with an initial velocity, and the projectile rebounds after colliding with the Martian surface. To ascertain the maximum height attained by the projectile after this collision, the known restitution coefficient and acceleration due to gravity are employed.
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Impact loading occurs when a moving object collides with a stationary structure, such as a rod with a uniform cross-sectional area fixed at one end. Under these conditions, the rod absorbs the kinetic energy from the striking object, leading to deformation and subsequent stress development. As the rod returns to its original position and reaches maximum stress, the absorbed energy, initially manifested as kinetic energy, transforms entirely into strain energy.
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Hypervelocity Impact Detection and Location for Stiffened Structures Using a Probabilistic Hyperbola Method.

Sunquan Yu1, Chengguang Fan1, Yong Zhao1

  • 1College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China.

Sensors (Basel, Switzerland)
|April 23, 2022
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Summary

This study introduces a new method to detect and locate hyper-velocity impacts on spacecraft using Lamb waves. The technique achieves high accuracy, with errors less than 1 cm for a 1-square-meter plate.

Keywords:
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Area of Science:

  • Aerospace Engineering
  • Materials Science
  • Wave Propagation

Background:

  • Hyper-velocity impacts (HVIs) from orbital debris pose a significant threat to spacecraft safety.
  • Accurate detection and localization of these impacts are crucial for spacecraft structural integrity and mission success.

Purpose of the Study:

  • To develop and validate a probabilistic method for detecting and locating HVIs in stiffened aluminum plates using Lamb wave analysis.
  • To investigate the characteristics of acoustic emission and shock wave propagation generated by HVIs.

Main Methods:

  • A hybrid model combining finite element analysis (FEA) and smoothed particle hydrodynamics (SPH) was employed for numerical simulations.
  • Experimental validation was performed using a two-stage light gas gun to simulate HVI conditions.
  • Lamb wave propagation and signal analysis were utilized for impact detection and localization.

Main Results:

  • The hybrid FEA-SPH model accurately predicted HVI-induced acoustic emission and shock wave propagation, showing quantitative agreement with experimental data.
  • Shock waves rapidly transform into Lamb waves, with the S0 mode dominating the signal energy (frequencies below 500 kHz).
  • The proposed method achieved an average location error of less than 1 cm for a 1-square-meter plate using only four sensors.

Conclusions:

  • The probabilistic Lamb wave analysis method is effective for detecting and locating HVIs in stiffened aluminum plates.
  • The study validates the hybrid FEA-SPH model for simulating HVI phenomena.
  • The findings contribute to enhanced spacecraft impact detection and monitoring systems.