logo
Buon prezzo  in linea

Dettagli dei prodotti

Created with Pixso. Casa Created with Pixso. prodotti Created with Pixso.
Parti di ceramica
Created with Pixso.

High-Performance Structural Foam for Aerospace and Composite Applications

High-Performance Structural Foam for Aerospace and Composite Applications

Marchio: ZMSH
MOQ: 100
Condizioni di pagamento: T/T
Informazione dettagliata
Luogo di origine:
SHANGHAI, CINA
Descrizione di prodotto

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.


High-Performance Structural Foam for Aerospace and Composite Applications 0High-Performance Structural Foam for Aerospace and Composite Applications 1

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:



Property Test Method Unit 30 RS 50 RS 75 RS 110 RS 200 RS
Density ISO 845 kg/m³ 30 50 75 110 200
Compression Strength ISO 844 MPa 0.40 0.85 1.70 3.60 9.50
Tensile Strength ASTM D638 MPa 0.80 1.68 2.30 3.70 7.00
Tensile Modulus ASTM D638 MPa 38 83 108 197 380
Elongation at Break ASTM D638 % 2.4 2.6 2.8 2.8 3.0
Flexural Strength ASTM D790 MPa 0.80 1.60 2.90 5.20 13.0
Shear Strength ASTM C273 MPa 0.40 0.85 1.25 2.38 5.00
Shear Modulus ASTM C273 MPa 15 30 48 80 160
Compressive Creep GB/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:


Density Size (mm) Standard Thickness (mm) Available Thickness (mm)
30 RS 2500×1250 4-80 1-120
50 RS 2500×1250 4-80 1-120
75 RS 2500×1250 4-65 1-100
110 RS 2160×1100 4-55 1-90

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.