Back to results

Embry Riddle Aeronautical University

Hypervelocity Impact Analysis of Hybrid Nanocomposite Sensors for Inflatable Space Structures

Abstract

dc:description.abstract

<p>Future space exploration requires easy-to-transport, and easy-to-build and deploy space habitats. NASA and Bigelow Aerospace have collaborated so that human habitation can be made safe and easy with inflatable space habitats (Litteken, 2017). One of the biggest threats faced by these structures in outer space is impact damage by micrometeoroid orbital debris (MMOD) traveling at velocities as high as 15 km/s (Lemmens, Krag, Rosebrock, & Carnelli, 2013). This work presents fabrication and testing of hybrid nanocomposites with carbon nanotubes (CNT) and coarse graphene nanoplatelets (GNP) as fillers and flexible epoxy matrix, that are proposed to be used for sensing the impact damage by MMOD in space inflatable structures. CNT and GNP were chosen as fillers owing to their excellent electrical properties and piezoresistivity. A new method was developed to cut graphite sheet (composed of GNPs) in laser marker and distribute it in patterns on carbon nanotube sheet (buckypaper) in epoxy matrix. Piezoresitivity tests were carried out and results were compared with percolation-based Monte Carlo simulations from past research. A hypervelocity impact test was designed and executed at the University of Dayton Research Institute, Ohio, to test the response of the sensors to hypervelocity impacts. Aluminum spheres of 3 mm diameter and 4.5 mm diameter were accelerated to 7 km/s and shot at the sensors, and results were recorded during and after the test. A periodic scanning multichannel control circuit was designed to power the sensors. LabVIEW codes were used for data acquisition and recognizing the location of the damage. The results proved that the hybrid CNT-GNP/epoxy nanocomposites can be used to create a damage detection system which would not only detect the impact damage caused by MMOD of 3mm diameter traveling at 7km/s but also discern its location and depth of penetration by the MMOD.</p>

Degree

thesis:*
Name thesis:degree_name
Master of Science in Aerospace Engineering
Level thesis:degree_level
Thesis - Open Access
Discipline thesis:degree_discipline
Aerospace Engineering
Year
2019

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Gola, Yachna

Subjects

dc:subject × 8

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/461
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1462

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Gola, Yachna. Hypervelocity Impact Analysis of Hybrid Nanocomposite Sensors for Inflatable Space Structures. Thesis - Open Access thesis, 2019. https://commons.erau.edu/edt/461