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HISTORICAL
1993-04-01
Standard
AIR1168/6
This section relates the engineering fundamentals and thermophysical property material of the previous sections to the airborne equipment for which thermodynamic considerations apply. For each generic classification of equipment, information is presented for the types of equipment included in these categories, and the thermodynamic design considerations with respect to performance, sizing, and selection of this equipment.
CURRENT
2011-07-25
Standard
AIR1168/6A
This section relates the engineering fundamentals and thermophysical property material of the previous sections to the airborne equipment for which thermodynamic considerations apply. For each generic classification of equipment, information is presented for the types of equipment included in these categories, and the thermodynamic design considerations with respect to performance, sizing, and selection of this equipment.
2016-09-10
WIP Standard
AIR1811B
The purpose of this Aerospace Information Report (AIR) is to provide guidelines for the selection and design of airborne liquid cooling systems. This publication is applicable to liquid cooling systems of the closed loop type and the expendable coolant type in which the primary function is transporting of heat from its source to a heat sink. Most liquid cooling system applications are oriented toward the cooling of electronics. Liquid cooling techniques, heat sinks, design features, selection of coolants, corrosion control, and servicing requirements for these systems are presented. Information on vapor compression refrigeration systems, which are a type of cooling system, is found in Reference 1.
HISTORICAL
1985-09-01
Standard
AIR1811
This publication is applicable to liquid cooling systems of the closed loop type and the expendable coolant type in which the primary function is transporting of heat from its source to a heat sink. Most liquid cooling system applications are oriented toward the cooling of electronics. Liquid cooling techniques, heat sinks, design features, selection of coolants, corrosion control, and servicing requirements for these systems are presented. Information on vapor compression refrigeration systems, which are a type of cooling system, is found in Reference 1.
CURRENT
1997-10-01
Standard
AIR1811A
This publication is applicable to liquid cooling systems of the closed loop type and the expendable coolant type in which the primary function is transporting of heat from its source to a heat sink. Most liquid cooling system applications are oriented toward the cooling of electronics. Liquid cooling techniques, heat sinks, design features, selection of coolants, corrosion control, and servicing requirements for these systems are presented. Information on vapor compression refrigeration systems, which are a type of cooling system, is found in Reference 1.
HISTORICAL
1956-12-01
Standard
AIR64
This AIR is intended as a status report on the of E.C.S. to date in dealing with the problem of equipment cooling in present and immediate future civil transport aircraft. Subsequent revisions to this AIR will follow as more information is gathered on this subject.
HISTORICAL
1998-01-01
Standard
AIR1277A
This document contains information on the cooling of modern airborne electronics, emphasizing the use of a heat exchange surface which separates coolant and component. It supplements the information contained in AIR64 for the draw through method and in AIR728 for high Mach Number aircraft. Report contents include basic methods, characteristics of coolants, application inside and outside of the black box use of thermostatic controls to improve reliability and system design. Characteristics of typical cooling components are treated sufficiently to permit selection and to estimate size and weight. While emphasis is placed herein on equipment cooling, section 10 dealing with thermal control of the environment, reminds the reader that some equipment will require heating for start up from a cold condition or as a means to control temperature within narrow limits (e.g. in a crystal oven). Property data and constants are also tabulated. All numerical values are given in British and SI units.
CURRENT
2005-02-09
Standard
AIR1277B
This SAE Aerospace Information Report (AIR) contains information on the thermal design requirements of airborne avionic systems used in military airborne applications. Methods are explored which are commonly used to provide thermal control of avionic systems. Both air and liquid cooled systems are discussed.
CURRENT
1999-03-01
Standard
AIR1191A
A general method for the preliminary design of a single, straight-sided, low subsonic ejector is presented. The method is based on the information presented in References 1, 2, 3, and 4, and utilizes analytical and empirical data for the sizing of the ejector mixing duct diameter and flow length. The low subsonic restriction applies because compressibility effects were not included in the development of the basic design equations. The equations are restricted to applications where Mach numbers within the ejector primary or secondary flow paths are equal to or less than 0.3.
2018-01-09
WIP Standard
J461_201801
Factors influencing the uses of wrought copper and copper alloys concern electrical conductivity, thermal conductivity, machinability, formability, fatigue characteristics, strength, corrosion resistance, the ease with which alloys can be joined, and the fact that these materials are nonmagnetic. Copper and its alloy also have a wide range of rich, pleasing colors. The only other metal with such distinctive coloring is gold. These materials are all easily finished by buffing, scratch brushing, plating or chemically coloring, or clear protective coating systems. When it is desired to improve one or more of the important properties of copper, alloying often solves the problem. A wide range of alloys, therefore, has been developed and commercially employed, such as the high copper alloys, brasses, leaded brasses, tin bronzes, heat treatable alloys, copper-nickel alloys, nickel silvers, and special bronzes. nickel silvers, and special bronzes.
CURRENT
2017-03-30
Standard
AMS4933F
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and flash welded rings up through 4.000 in2 (25.81 cm2) cross-section and stock for flash welded rings.
CURRENT
2014-10-27
Standard
AMS4937D
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings up through 4.00 inches (101.6 mm) in diameter or least distance between parallel sides and stock for flash welded rings.
2017-09-22
WIP Standard
AMS4937E
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings and stock for flash welded rings.
CURRENT
2016-06-16
Standard
AMS4955H
This specification covers a titanium alloy in the form of welding wire.
CURRENT
2015-01-15
Standard
AMS4950D
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging or flash welded rings of any size (See 8.6).
CURRENT
2015-12-04
Standard
AMS4952F
This specification covers a titanium alloy in the form of welding wire.
CURRENT
2015-12-04
Standard
AMS4953G
This specification covers a titanium alloy in the form of welding wire.
CURRENT
2016-08-01
Standard
AMS4963D
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings up through 3.999 inches (101.57 mm), inclusive and stock for forging, flash welded rings, or heading.
CURRENT
2016-02-02
Standard
AMS5585H
This specification covers a corrosion and heat resistant alloy in the form of welded and drawn tubing.
CURRENT
2015-12-05
Standard
AMS5567F
This specification covers a corrosion-resistant steel in the form of seamless or welded tubing.
CURRENT
2016-05-16
Standard
AMS5558H
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
CURRENT
2016-08-01
Standard
AMS4973H
This specification covers a titanium alloy in the form of forgings up to 4.000 inches (101.60 mm) inclusive and forging stock.
CURRENT
2017-10-20
Standard
AMS5031G
This specification covers a low-carbon steel in the form of covered welding electrodes.
CURRENT
2015-09-16
Standard
AMS5034B
This specification covers a low-alloy steel in the form of welding wire.
CURRENT
2014-12-23
Standard
AMS5035C
This specification covers a low-alloy steel in the form of welding wire.
HISTORICAL
1981-07-01
Standard
AMS4397
CURRENT
1996-09-01
Standard
AMS4397A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: LA141A UNS Number: M14141
CURRENT
2017-05-30
Standard
AMS4416B
This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness (see 8.5).
HISTORICAL
2012-03-10
Standard
AMS4459
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with cross sectional area of 22.5 square inches (145 cm2) maximum and a circumscribing circle diameter (circle size) of 17.4 inches (44.2 cm) maximum. See 8.3 for definition of circumscribing circle size.
CURRENT
2013-01-03
Standard
AMS4459A
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with cross sectional area of 22.5 square inches (145 cm2) maximum and a circumscribing circle diameter (circle size) of 17.4 inches (44.2 cm) maximum. See 8.3 for definition of circumscribing circle size.
Viewing 1 to 30 of 536

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