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| اسم العلامة التجارية: | ZMSH |
| الـ MOQ: | 100 |
| شروط الدفع: | تي/تي |
High-Performance Structural Foam for Aerospace and Composite Applications
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.
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
| 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.
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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