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SAE Aerospace Technical Papers Collection

2016-11-30

The Aerospace Technical Paper Collection is a family of technical papers as either an annual subscription (current papers, archived papers, or both) or a perpetual collection (1906-1997). This collection is perfect for aerospace engineers, managers, or educators who need access to the most current content covering today's most relevent topics. Please contact one of our sales representatives to learn more and start your subscription today! SAE Sales Team customersales@sae.org 1-888-875-3976 (U.S. and Canada) 1-724-772-4086 (Outside the U.S.)

Magazine

Quantity Order Aero Engrg

1987-11-01

Standard

Steel Tubing (Seamless for Machined Parts) 1.8ni 0.80cr 0.25mo (0.38 - 0.43c) Heat Treated (200,000 Tensile Strength)

2002-12-16

CURRENT

AMS6420

Standard

STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)

1942-06-01

HISTORICAL

AMS6510

Standard

Steel Tubing (Seamless) Round 0.55ni 0.5cr 0.2mo (0.27 - 0.33c) Heat Treated (125,000 Tensile Strength)

2002-12-16

CURRENT

AMS6531

Standard

STEEL Nickel Molybdenum

1939-12-04

HISTORICAL

AMS6315

Standard

Steel 1.8ni .25mo (0.38 - 0.43c) Heat Treated (105,000 Tensile Strength)

1946-08-01

CURRENT

AMS6315C

No scope available.

Standard

STEEL Nickel Molybdenum

1942-03-01

HISTORICAL

AMS6315A

Standard

STEEL 1.8 Ni - .25 Mo (.38 - .43C) Heat Treated (105,000 TS)

1945-07-01

HISTORICAL

AMS6315B

Standard

Steel Tubing (Seamless for Machined Parts) .55ni .25mo (.33 - .38c) Normalized Or Heat-Treated (90,000 Tensile Strength)

2002-12-16

CURRENT

AMS6283

Standard

Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.35 - .38c) Heat-Treated (125,000 Tensile Strength)

2002-12-16

CURRENT

AMS6284

Standard

Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.38 - .43c) Heat-Treated (180,000 Tensile Strength)

2002-12-16

CURRENT

AMS6285

Standard

Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (125,000 Tensile Strength)

2002-12-16

CURRENT

AMS6366

Standard

Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (150,000 Tensile Strength)

2002-12-16

CURRENT

AMS6367

Standard

Steel Tubing, (Seamless), Round Chromium Molybdenum (.32 - .39 Carbon) (200,000 Tensile Strength)

2002-12-16

CURRENT

AMS6368

Standard

Steel Tubing (Seamless), Round Chromium Molybdenum (0.27 - 0.33 Carbon) (180,000 Tensile Strength - 0.156 Maximum Wall Thickness)

2002-12-16

CURRENT

AMS6363

Standard

BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded

1973-05-15

HISTORICAL

AMS7461B

This specification covers premium quality bolts and screws made of 6Al - 4V titanium alloy.

Standard

BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded

1970-11-01

HISTORICAL

AMS7461A

Standard

BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded

1964-06-30

HISTORICAL

AMS7461

Standard

COMMUNICATIONS MANAGEMENT UNIT (CMU) MARK 2

2019-11-26

CURRENT

ARINC758-4

This ARINC Standard specifies the ARINC 758 Mark 2 Communications Management Unit (CMU) as an on-board message router capable of managing various datalink networks and services available to the aircraft. Supplement 4 adds Ethernet interfaces, per ARINC Specification 664 Part 2. This will allow the CMU to communicate with IP based radio transceivers (e.g., L-Band Satellite Communication Systems (Inmarsat SwiftBroadband (SBB) and Iridium Certus), ACARS over IP, AeroMACS, etc.).