Paper #96190

Paper information

Paper code: IAC-25,C4,4,4,x96190
Date: 2025-10-01
Time: 11:01
Order: 4
Room: Room C4.11
Title: Study of potential use of Magnesium/Teflon/Viton Pyrotechnic Composition as an ignitor for solid rocket motors through computational simulations using molecular dynamics (MD).
abstract: View PDF
Session: 4. Solid and Hybrid Propulsion (2)
symposium: C4. IAF SPACE PROPULSION SYMPOSIUM
congress: IAC-25
Type of presentation: oral

Main author: Mr. Vinicius Rossetto, Instituto Tecnológico de Aeronáutica (ITA), Brazil

Co-authors

Prof. Rene Gonçalves, Aeronautic Institute of Technology (ITA), Brazil;

Prof.Dr. José Rocco, ITA-DCTA, Brazil;