Document ID:	ASTM-E2581       Scroll down to access document images

Overview

Title:  Polymer Matrix Composites, Shearography of, Sandwich Core Materials and Filament-Wound Pressure Vessels in Aerospace Applications Scope:  This practice describes procedures for shearography of polymer matrix composites, sandwich core materials, and filament-wound pressure vessels made entirely or in part from fiber-reinforced polymer matrix composites. The composite materials under consideration typically contain continuous high modulus (greater than 20 GPa (3106 psi)) fibers, but may also contain discontinuous fiber, fabric, or particulate reinforcement. Status:  Active Adoption Date:  26-JAN-2010         Next Review Due:  27-FEB-2028 FSC/Area:  NDTI Doc Category:   American Society for Testing and Materials (ASTM)   Reaffirmation Date:  01-MAR-2018

Responsibilities

Lead Standardization Activity:  MR  Army Research Laboratory, Weapons and Materials Research Directorate     Adopting Activity: 20  Air Force Research Laboratory (AFRL) Coordination:  Full   Army Custodian:  MR   Army Research Laboratory, Weapons and Materials Research Directorate   Navy Custodian:  AS   Naval Air Systems Command   Air Force Custodian:  20   Air Force Research Laboratory (AFRL)

Revision History

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