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High-Performance Structural Foam for Aerospace and Composite Applications

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High-Performance Structural Foam for Aerospace and Composite Applications

High-Performance Structural Foam for Aerospace and Composite Applications


Product Description:


This high-performance structural foam is designed for aerospace applications, including rocket fairings, interstage sections, and large aircraft aft pressure frames. Its excellent mechanical and thermal properties also make it ideal for helicopter main rotor blades, tail rotor blades, and fuselage panels.


The rigid foam can withstand processing conditions up to 0.3 MPa at 180 °C, and after thermal treatment, it can reach 0.7 MPa at 180 °C. This makes it perfectly suited for autoclave curing, molding processes, and various resin injection techniques.


Key Features:


  • Wide density range: 30 kg/m³ to 200 kg/m³

  • High compression, tensile, bending, and shear strength

  • Excellent thermal stability and heat resistance

  • Suitable for high-temperature autoclave and molding processes

  • Ideal for aerospace and helicopter structural components


Technical Specifications:



PropertyTest MethodUnit30 RS50 RS75 RS110 RS200 RS
DensityISO 845kg/m³305075110200
Compression StrengthISO 844MPa0.400.851.703.609.50
Tensile StrengthASTM D638MPa0.801.682.303.707.00
Tensile ModulusASTM D638MPa3883108197380
Elongation at BreakASTM D638%2.42.62.82.83.0
Flexural StrengthASTM D790MPa0.801.602.905.2013.0
Shear StrengthASTM C273MPa0.400.851.252.385.00
Shear ModulusASTM C273MPa15304880160
Compressive CreepGB/T 15048%≤2.0////
Heat Deflection Temp.DIN 53424°C≥200////


Processing Conditions for Compressive Creep Test:


  • 30 RS: 130 °C / 0.1 MPa / 2h

  • 50 RS: 130 °C / 0.3 MPa / 2h

  • 75 RS: 150 °C / 0.3 MPa / 2h

  • 110 RS: 180 °C / 0.3 MPa / 2h


Standard Panel Sizes & Thickness:


DensitySize (mm)Standard Thickness (mm)Available Thickness (mm)
30 RS2500×12504-801-120
50 RS2500×12504-801-120
75 RS2500×12504-651-100
110 RS2160×11004-551-90

Tolerance: Thickness ±0.2 mm; other tolerances available upon request.


FAQ


1: What temperature and pressure can this structural foam withstand?

  • The foam can withstand processing conditions up to 0.3 MPa at 180 °C. After thermal treatment, it can reach 0.7 MPa at 180 °C, making it ideal for autoclave curing, molding, and resin injection processes.


2: What aerospace components is this foam suitable for?

  • This foam is suitable for rocket fairings, interstage sections, large aircraft aft pressure frames, as well as helicopter main rotor blades, tail rotor blades, and fuselage panels.


3: What sizes and thicknesses are available?

  • Standard panel sizes range from 2160×1100 mm to 2500×1250 mm. Thickness can be customized from 1 mm to 120 mm depending on density, with a standard tolerance of ±0.2 mm. Other tolerances are available upon request.


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