ASTM-D5687 › Standard Guide for Preparation of Flat Composite Panels with Processing Guidelines for Specimen Preparation
The following bibliographic material is provided to assist you with your purchasing decision:
Scope
1.1 This guide provides guidelines to facilitate the proper preparation of laminates and test specimens from fiber-reinforced organic matrix composite prepregs. The scope is limited to organic matrices and fiber reinforcement in unidirectional (tape) or orthagonal weave patterns. Other forms may require deviations from these general guidelines. Other processing techniques for test coupon preparation, for example, pultrusion, filament winding and resin-transfer molding, are not addressed.
1.2 Specimen preparation is modeled as an 8-step process that is presented in and Section . Laminate consolidation techniques are assumed to be by press or autoclave. This practice assumes that the materials are properly handled by the test facility to meet the requirements specified by the material supplier(s) or specification, or both. Identification and information gathering guidelines are modeled after Guide E 1309. Test specimens shall be directly traceable to material used as designated in Guide E 1434. Proper test specimen identification also includes designation of process equipment, process steps, and any irregularities identified during processing.
1.3 The values stated in either SI units or inch-pound units are to be regarded separately as standard. Within the text the inch-pound units are shown in brackets. The values stated in each system are not exact equivalents; therefore, each system must be used independently of the other. Combining values from the two systems may result in nonconformance with the standard.
1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Keywords
composite materials; laminates; panel preparation; polymer matrix composites; specimen preparation; ICS Number Code 83.140.10 (Films and sheets)
To find similar documents by ASTM Volume:
15.03 (Space Simulation; Aerospace and Aircraft; Composite Materials)
To find similar documents by classification:
83.140.10 (Films and sheets Including plates)
This document comes with our free Notification Service, good for the life of the document.
This document is available in either Paper or PDF format.
Customers who bought this document also bought:
NAS-410NAS Certification and Qualification of Nondestructive Test Personnel
AWS-D17.1/D17.1M
Specification for Fusion Welding for Aerospace Applications
MIL-H-7199
Heat Treatment of Wrought Copper-Beryllium Alloys, Process for (Copper Alloys: Numbers C17000, C17200, C17300, C17500, and C17510) (Superseded by SAE-AMS-H-7199)
Document Number
ASTM-D5687_D5687M-20
Revision Level
2020 EDITION
Status
Current
Modification Type
Reapproval
Publication Date
Nov. 6, 2020
Document Type
Guide
Page Count
16 pages
Committee Number
D30.04