Items |
7075-T651-250-485-1445 Aluminum Plate - Series 7075-T651 |
7075-T651-313-485-1445 Aluminum Plate - Series 7075-T651 |
7075-T651-375-485-1445 Aluminum Plate - Series 7075-T651 |
7075-T651-500-485-1445 Aluminum Plate - Series 7075-T651 |
7075-T651-750-485-1445 Aluminum Plate - Series 7075-T651 |
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Material | N/A Aluminum | |||||||||
Shapeform | N/A Plates | |||||||||
Series | N/A 7075-T651 | |||||||||
Grade | N/A 7075 | |||||||||
Preparation | N/A Interleaved and Stenciled | |||||||||
Temper | N/A T651 | |||||||||
Finish | N/A Mill | |||||||||
Thickness | N/A 0.25 inches6.3500 mm | N/A 0.313 inches7.9502 mm | N/A 0.375 inches9.5250 mm | N/A 0.500 inches12.7 mm | N/A 0.750 inches19.05 mm | |||||
Size | N/A 48.5 x 144.5 | |||||||||
Width | N/A 48.5 | |||||||||
Length | N/A 144.5 | |||||||||
Sheet Weight per Unit Area | N/A 3.636 lbs/ft²17.750952 kg/m² | N/A 4.552 lbs/ft²22.222864 kg/m² | N/A 5.454 lbs/ft²26.626428 kg/m² | N/A 7.272 lbs/ft²35.501904 kg/m² | N/A 10.908 lbs/ft²53.252856 kg/m² | |||||
Weight per Plate | N/A 176.96 lbs80.16288 kg | N/A 221.55 lbs100.36215 kg | N/A 265.44 lbs120.24432 kg | N/A 353.92 lbs160.32576 kg | N/A 530.87 lbs240.48411 kg | |||||
ASTM Specification | N/A AMS-QQ-A250/12 ASTM B209 | |||||||||
Ultimate Strength | N/A 83 ksi | |||||||||
Yield Strength | N/A 73 ksi | |||||||||
Elongation percent in 2 inches | N/A 11 | |||||||||
Hardness Brinnel Number | N/A 150 | |||||||||
Ultimate Shearing Strength | N/A 48 ksi | |||||||||
Fatigue Endurance Limit1 | N/A 23 ksi | |||||||||
Modulus of Elasticity2 | N/A 10.4 x 102 ksi | |||||||||
Resistance to Corrosion - General3 | N/A C | |||||||||
Stress Corrosion Cracking4 | N/A C | |||||||||
Workability (Cold)5 | N/A D | |||||||||
Mechinability | N/A B | |||||||||
Brazeability6 | N/A D | |||||||||
Gas Weldability7 | N/A D | |||||||||
Arc Weldability8 | N/A D | |||||||||
Resistance Spot and Seam Weldability9 | N/A B | |||||||||
Applications | N/A Aircraft and other structures | |||||||||
Density | N/A 0.101 lbs/in³ | |||||||||
Specific Gravity | N/A 2.81 | |||||||||
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