Documents
Materials Crashworthiness Advanced Manufacturing Lightning
- 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]
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [US Units]
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [US Units]
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700SC-12K-50C/#2510 Plain Weave Fabric [SI Units]
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [SI Units]
- ABasis and BBasis Design Allowables for EpoxyBased Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [SI Units]
- Laminate Design Allowables for TORAY T700G/#2510 Unidirectional Tape, T700S/#2510 Plain Weave Fabric and 7781 Finish 558/#2510 Fiberglass Fabric
- 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)
- 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
- Design and Construction of a Crashworthy Composite Airframe
- Crashworthiness Design Guide Small Airplane Small Airplane
- Full-Scale Starship Test