Fabrication of Sandwich Panels for Weight Portable Shelters

Radomes, Foam Sandwich Polyimide/Quartz Cloth Construction

Radome, Foam Sandwich Hot-Melt, Addition-Type Polyimide

Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric

Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - Glass Fiber and Epoxy Resin, 7781 Weave Fabric

Acceptance Criteria Adhesive-Bonded Metal-Faced Sandwich Structures

Plywood, Medium Density

Plywood, High Density

Fiberboard, Hard-Pressed, Structural

Rubber: Butyl (IIR) Low Compression Set and Low Moisture/Gas Permeability 65 to 75 Type A Hardness for Applications Requiring Resistance to Gas and/or Water Vapor Permeation

Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape

350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs

350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 38, Class 2, Grade 193, Style 3K-70-PW, Fiber 1

350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 2

350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 1

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 0 - Introduction

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive, and Non-Structural Glass Prepreg

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 3 - Purchasing Specification for Carbon Prepreg

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 4 - Purchasing Specification for Film Adhesive

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 5 - Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinforced Epoxy Prepreg for Repair, Plain Weave Fabric, 193 g/m2, Adhesive Film for Repair and Non-Structural Glass Fiber Fabric Reinforced Epoxy Prepreg, 105 g/m2

Aluminum Sheet and Plate (1060-0)

Aluminum Sheet and Plate, 0.12Cu (1100-0), Annealed

Aluminum Alloy Tubing, Seamless, Drawn 1.8Cu - 1.0Mg - 0.8Si - 0.20Cr Solution Heat Treated, Stress-Relieved by Stretching, and Aged (2013-T6511)