17,005 Documents in our Technical Library
3180521 Total Downloads

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

AGATE-WP3.3-033048-116

AGATE-WP3.3-033048-116
  • Version
  • 217 Downloads
  • 856.59 KB File Size
  • 1 File Count
  • August 8, 2016 Create Date
  • August 8, 2016 Last Updated
Scroll for Details

Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems

AGATE-WP3.3-033048-116 Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems

The purpose of this qualification plan is to describe an acceptable program to
substantiate that the materials and processes employed meet appropriate
Federal Aviation Administration (FAA) requirements. These requirements apply
to the original material qualification. Once certified, changes to the material,
process, tooling and/or facility require a review and it may be required that some
(or all) of these tests be repeated.

This plan gives specific information about the qualification program for a
2x2 biaxially braided composite material system that is manufactured
using a Resin Transfer Molding (RTM) process. Specifically, this plan
covers one-part resin systems which are premixed at the resin
manufacturer and combined with a braided sock preform via a RTM
process.

The qualification plan describes material qualification methodology for a
2x2 biaxially braided composite material system that is manufactured
using a resin transfer molding (RTM) process. Additionally, this plan
establishes testing methods and process controls necessary to certify
composite materials used for airframe components under FAR Part 23
requirements. In some cases, unique characteristics of a material system
or its application may require testing beyond that described in this
document. In these situations, Aircraft Certification Offices (ACOs) may
require additional testing to demonstrate compliance to the applicable
Federal Aviation Regulations (FARs).

FileAction
AGATE-WP3.3-033048-116 Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

AGATE-WP3.3-033048-116

AGATE-WP3.3-033048-116
  • Version
  • 217 Downloads
  • 856.59 KB File Size
  • 1 File Count
  • August 8, 2016 Create Date
  • August 8, 2016 Last Updated
Scroll for Details

Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems

AGATE-WP3.3-033048-116 Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems

The purpose of this qualification plan is to describe an acceptable program to
substantiate that the materials and processes employed meet appropriate
Federal Aviation Administration (FAA) requirements. These requirements apply
to the original material qualification. Once certified, changes to the material,
process, tooling and/or facility require a review and it may be required that some
(or all) of these tests be repeated.

This plan gives specific information about the qualification program for a
2x2 biaxially braided composite material system that is manufactured
using a Resin Transfer Molding (RTM) process. Specifically, this plan
covers one-part resin systems which are premixed at the resin
manufacturer and combined with a braided sock preform via a RTM
process.

The qualification plan describes material qualification methodology for a
2x2 biaxially braided composite material system that is manufactured
using a resin transfer molding (RTM) process. Additionally, this plan
establishes testing methods and process controls necessary to certify
composite materials used for airframe components under FAR Part 23
requirements. In some cases, unique characteristics of a material system
or its application may require testing beyond that described in this
document. In these situations, Aircraft Certification Offices (ACOs) may
require additional testing to demonstrate compliance to the applicable
Federal Aviation Regulations (FARs).

FileAction
AGATE-WP3.3-033048-116 Material Qualification Methodology for 2X2 Biaxially Braided RTM Composite Material Systems.pdfDownload 
17,005 Documents in our Technical Library
3180521 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...