Materials Crashworthiness Advanced Manufacturing Lightning
AGATE History
AGATE Shared Database Process
In recent years, NASA, industry and the FAA have worked together to help the aviation
industry deliver more aircraft in less time by sharing central material qualification
databases. This concept was first tested with the databases formed through the Advanced
General Aviation Transport Experiments (AGATE), formed by NASA in 1995 and led by
NIAR at WSU. The purpose of AGATE was to develop affordable new technology, industry
standards and certification methods for general aviation aircraft.
Before AGATE, the traditional approach to qualifying materials meant individual companies used "customized" qualification programs, leading to detailed and expensive procedures for each company. Costs increased further as other procedures were established for structural testing, manufacturing control and repair. As a result, most programs were limited to using materials previously qualified for other programs, which led to using older, outdated material and not taking advantage of the latest technology and material advances in the industry.
With the creation of AGATE, the AGATE Shared Database Process was formed. The shared databases created using the AGATE process allowed a manufacturer to select a pre-approved composite material system to fabricate parts through a smaller subset of testing for a specific application (known as equivalency). The materials accepted into these shared databases required that the raw materials be manufactured in accordance with process control documents and material specifications, which impose control of the key physical, chemical and mechanical properties of the material.
Through the joint collaboration of two government agencies, NASA and FAA, AGATE was able to reduce the time required for certification of new composite materials by a factor of four and the cost of certification by a factor of 10. The timeline below highlights the progress AGATE made, leading to NCAMP.
Materials
- Material Qualification and Equivalency for Polymer Matrix Composite Material Systems (Updated Sept. 2003)
- [AGATE Statistical Analysis Program (ASAP) 2004 -Version 1]
Latest versions are available through NCAMP site - Material Qualification Methodology for 2x2 Biaxially Braided RTM Composite Material Systems
- Material Qualification Methodology for Field Repair/Wet Layup Composite Material Systems
- B-Basis design Allowables for Epoxy-Based Prepreg: Newport Carbon Plain Weave Fabric 3K70P/NB321
- B-Basis design Allowables for Epoxy-Based Prepreg: Newport Graphite Unitape G150 NASS/NCT321
- B-Basis design Allowables for Epoxy-Based Prepreg: Newport E-Glass Fabric 7781/NB321
- B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally 3M) E-Glass Fabric 7781/SP381
- B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally 3M) S-Glass Unitape S2/SP381
- B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) Plain Weave Graphite Fabric T650 3K-70-PW/7740
- B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) Graphite Unitape G30-500 12K/7740
- B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) 8-Harness Graphite Fabric T650 3K-135-8H/7740
- B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 3KPW/E765
- B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) Graphite Unitape T700 24KP/E765
- B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) E-Glass Fabric 7781/E765
- Laminate Design Allowables for EpoxyBased Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 3KPW/E765
- Laminate Design Allowables for EpoxyBased Prepreg: Nelcote (formerly FiberCote) Graphite Fabric E765/T300 6K 5HS
- B-Basis Design Allowables for Wet Layup Field Repair Fiber Reinforced Composite Material Systems: 7781 Glass Fabric/MGS 418
- B-Basis Design Allowables for Wet Layup/Field Repair Fiber Reinforced Composite Material Systems: 3K Plain Weave Carbon Cloth/MGS 418
- B-Basis Design Allowables for 2x2 Biaxially Braided RTM Composite Material Systems: Carbon Braid AS4 6K GP/PR520
- BBasis Design Allowables for EpoxyBased Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 6K 5HS/E765
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700SC-12K-50C/#2510 Plain Weave Fabric [US Units] - SAE AMS3914
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [US Units] - SAE AMS3960
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [US Units] - SAE AMS3915
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700SC-12K-50C/#2510 Plain Weave Fabric [SI Units] - SAE AMS3914
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [SI Units] - SAE AMS3960
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [SI Units] - SAE AMS3915
- Laminate Design Allowables for TORAY T700G/#2510 Unidirectional Tape, T700S/#2510 Plain Weave Fabric and 7781 Finish 558/#2510 Fiberglass Fabric - SAE AMS3960, SAE AMS3914 and SAE AMS3915
- Investigation of Thick Bondline Adhesive Joints
- Effects of Surface Preparation on Long-Term Durability of Composite Adhesive Bonds
- Stress Analysis of In-Plane, Shear-Loaded, Adhesively Bonded Composite Joints and Assemblies
- Impact of Aircraft Operation on Composite Airframe Temperatures (THERMOD)
Crashworthiness
- Design and Test of an Improved Crashworthiness Small Composite Airframe
- Methodology for Seat Design and Certification by Analysis
- Test Plan - Impact Test of a General Aviation Composite Airframe
- Estimation of Firewall Loads due to Soft Soil Impact
- AGATE Composite Airframe Impact Test Results (Video 1) (Video 2)
- Design and Construction of a Crashworthy Composite Airframe
- Crashworthiness Design Guide Small Airplane Small Airplane
- Full-Scale Starship Test
Advanced Manufacturing
- Guide for Low Cost Design and Manufacturing of Composite General Aviation Aircraft
- Automotive Approaches for General Aviation Aircraft