Propellant cohesive fracture during the peel test of a propellant/liner structure
Author:
Affiliation:
1. Laboratoire PIMM, ENSAM, CNRS, CNAM, Paris, France
2. Airbus Safran Launchers, Centre de recherche du Bouchet, Vert-le-Petit, France
3. LMS, Ecole Polytechnique, CNRS, Université Paris-Saclay, Palaiseau, France
Funder
Direction Générale de l'Armement
Publisher
Informa UK Limited
Subject
Materials Chemistry,Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanics of Materials,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/00218464.2017.1332999
Reference21 articles.
1. Studies on Interface Properties of Propellant Liner for Case-Bonded Composite Propellants
2. Review of the Adhesively Bonded Interface in a Solid Rocket Motor
3. Cohesive Zone Modeling of Propellant and Insulation Interface Debonding
4. Experimental and numerical analysis of mode II fracture between propellant and insulation
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