6061 aluminum density chart

    • [DOC File]1 - Purdue University

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      The bumper we have created is designed for impacts above 7 km/s. It uses a 2 mm aluminum 6061 bumper and a 1.5 cm back wall layer of Kevlar. Having a separate layer for the back wall instead of using the structural aluminum adds safety. Kevlar’s high strength protects better then aluminum and adds less weight then aluminum.


    • [DOC File]IDE 120 – HARDNESS TESTING

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      C11000-H2 Copper Rockwell B: 40 41.2 5/8"x6" blue 6061-T651 Aluminum Brinell: 95 Rockwell B: 60 45 1/2"x3"x3" 5/8"x6" blue-green, AL 6061 C36000-H1 Brass Rockwell B: 62 55.8 1/2"x3"x3" 5/8"x6" orange, BRS 36000 A36 Hot-Rolled Steel Brinell: 119-159 Rockwell B: 67-83 71 (58-80 is common) 1/2"x3"x3"


    • [DOC File]Section

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      Consists of clear anodized aluminum. Outside diameter shall be 4.5 inches. 11 foot length . 6061-T6 aluminum alloy . Shaft wall 0.337 inch thick and weighing 5.18 lbs./ft.. ANSI B2.1 threads. Spun finished. RCS HEAD . Comply with MnDOT 3834 and the following supplements or modifications:


    • [DOC File]AAE 451 Aircraft Design - Purdue University

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      Material Thickness of skin (in) Total Weight (lbs) Aluminum 6061 T6 1.67E-03 0.007 Balsa 1.48E-01 0.593 Bass 1.64E-02 0.066 Spruce 1.50E-02 0.06 Table #2. As it can be seen the best material for the skin of our wing is aluminum. Since it is very strong, the thickness is very small and the weight as well.


    • [DOC File]Edition 2009 - State

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      Item Test Method Type or Grade Galvanizing Aluminum Materials (other than bracket) 911.01.01 Bracket B308 6061-T6 Structural steel shapes ASTM A709 Grade 36 ASTM A123 Steel Sheet ASTM A1011 Grade 36 ASTM A 653 Bolts (except special bolt for coupling) ASTM A325 ASTM A153 Special bolt for coupling ASTM A449 ASTM A153 Cap Screw ASTM A307 ASTM A153 ...



    • [DOC File]www.mrrace.com

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      Construction is of 6061-T6 aluminum sheet metal riveted to aluminum angles with. Avex rivets. This high strength aluminum alloy construction provides long life and low. maintenance costs thanks to its durability and corrosion resistance characteristics. Wings: The wing has a high lift airfoil with full-span fixed leading edge slats (bolted to ...


    • [DOCX File]Welcome to Indian Space Research Organisation

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      RATE CONTRACT FOR ANODIZING, BLACK ANODIZING, HARD ANODIZING ON ALUMINIUM ALLOY (AA 6061) COMPONENTS OF SPACECRAFT PROJECTS. Scope of the Rate Contract and Period of Contract: ISRO Satellite Centre (ISAC) is carrying out Anodizing, Black Anodizing and Hard anodizing coatings on AA6061 components for Indian Satellite program.


    • YORK CUSTOM GUIDE SPECIFICATION

      [Type 6061 T6 welded structural aluminum, [6-inch, 8-inch, 10-inch, 12-inch] ... Provide submittals with Cross plot table and chart with selected DX coil and Condensing unit provided. ... Filler material shall be inorganic glass fiber of a proper density to obtain the specified acoustic performance and be packed under not less than 5% ...


    • [DOC File]Memo - EDGE

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      The design of our thermal bridge consists of a 0.5 in diameter 6061-T6 aluminum rod that is exposed to the interior of the combustion chamber of the stove by a length of 1.5 in. ... area 2.34062E-05 m2 orifice diameter 0.0047625 m orifice area 5.67035E-06 m2 total orifice area 0.000175781 Air density 1.205 kg/m3 Air specific velocity 0.00001511 ...


    • [DOC File]Colorado Space Grant Consortium

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      The tensile yield stress of 6061-T6 Aluminum is 37 ksi. The compressive yield stress of 6061-T6 Aluminum is 37 ksi. The shear yield stress of 6061-T6 Aluminum is 19 ksi. Lexan Standoffs: Density: 0.94 kg/dm^3. Mass of plate: 0.4 lbs. Mass of standoff: 0.003481 lbs. Mass of system: 2.08 lbs. Mass allotted for experiments: 7.92 lbs. Mass per ...


    • [DOC File]Duo-Gard Industries Inc

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      Shall be extruded aluminum alloy of 6063-T5, 6005-T5 or 6061-T6 ASTM B 221. All sections shall be formed true to detail and free from defects impairing appearance, strength and durability. Provide integral weep holes in factory supplied extrusions and welded corner assemblies to provide end damns where applicable.


    • [DOC File]CONTENTS

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      Spatial density plots, shown in Figure 2, can be used to estimate the amount of debris in space. Spatial density is the number of objects per unit volume of space. ... Table 2 is a chart of the physical properties of the Ni-Cd batteries produced by Haowei.32. ... which is in this case aluminum. 6061-T6 aluminum has a thermal conductivity (k) of ...


    • [DOC File]OVERVIEW

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      Figure 2 contains a chart which shows the various polarization resistance values obtained for each area ratio of 304 stainless steel to 6061-T6 aluminum. The Acceptance Tests Results and Report document (Volume 3) contains data from all the experiments that were conducted during the course of the project.


    • [DOC File]THE FLOATING DUTCHMEN - RPI

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      2 $9.66 $19.32 - MSC: 02629335 Alloy 6061 Aluminum Material: Aluminum - Alloy 6061 Diameter: 1 Length: 12 1 $7.56 $7.56 - MSC: 32012254 Alloy 6061 Aluminum Material: Aluminum - Alloy 6061 Length: 72 Length: 6 Thickness: 1/4 Width: 1 1 $12.38 $12.38 - N/A Brass 1.6 lb $6 per lb $10.00 $10.00 Raw Materials Total $49.26 $10.00 Labor Costs Name ...


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