Standard
Wire, Steel, High Carbon, Round, Type I
2001-05-01
HISTORICAL
AMSQQW428/1
Search Results
Standard
Wire, Steel, Carbon (High Carbon, Round, For Mechanical Springs, General Purpose)
2013-04-03
HISTORICAL
AMSQQW428A
This specification covers uncoated, round, high carbon steel wire for the fabrication of mechanical springs and wire forms for general purpose use.
Standard
Wire, Steel, Carbon (High Carbon, Round, For Mechanical Springs, General Purpose)
2017-08-07
CURRENT
AMSQQW428B
This specification covers uncoated, round, high carbon steel wire for the fabrication of mechanical springs and wire forms for general purpose use.
Standard
Wire, Steel, Carbon (High Carbon, Round, For Mechanical Springs, General Purpose)
1998-12-01
HISTORICAL
AMSQQW428
This specification covers uncoated, round, high carbon steel wire for the fabrication of mechanical springs and wire forms for general purpose use.
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Tin-Coated Copper Conductor, 600-Volt, 110°C
2017-12-07
CURRENT
AS50861/5A
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Tin-Coated Copper Conductor, 600-Volt, 110°C
2012-12-12
HISTORICAL
AS50861/5
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Silver-Coated Copper Alloy Conductor, 600-Volt, 110°C
2018-01-02
CURRENT
AS50861/6A
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Silver-Coated Copper Alloy Conductor, 600-Volt, 110°C
2012-12-12
HISTORICAL
AS50861/6
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-PVC-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C
2012-12-12
HISTORICAL
AS50861/3
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-PVC-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C
2017-12-07
CURRENT
AS50861/3A
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C
2012-12-12
HISTORICAL
AS50861/2
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, Medium Weight, 600-Volt, 105°C
2012-04-04
HISTORICAL
AS50861/7
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 600-Volt, 105°C
2012-04-04
HISTORICAL
AS50861/1
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 3000-Volt, 105°C
2018-02-06
CURRENT
AS50861/4A
Standard
Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 3000-Volt, 105°C
2012-12-12
HISTORICAL
AS50861/4
Standard
Wire, Electrical, Insulated, Antenna
2008-03-25
HISTORICAL
AS6370
This specification covers insulated wire for use in external aircraft antennas.
Standard
Wire, Electrical, Insulated, Antenna
2014-05-01
CURRENT
AS6370A
This specification covers insulated wire for use in external aircraft antennas.
Standard
Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy
2001-07-01
HISTORICAL
AS22759
This specification covers fluoropolymer-insulated single conductor electrical wires made with tin-coated, silver-coated, or nickel-coated conductors of copper or copper alloy as specified in the applicable specification sheet. The fluoropolymer insulation of these wires may be polytetrafluoroethylene (PTFE), fluorinated ethylene propylene (FEP), polyvinylidene fluoride (PVF2), ethylene-tetrafluoroethylene copolymer (ETFE), or other fluoropolymer resin. The fluoropolymer may be used alone or in combination with other insulation materials.
Technical Paper
Wing-Lift Augmentation Methods for the Improvement of Low-Speed Performance of High-Speed Aircraft
1956-01-01
560012
FOR more than half a century, aeronautical researchers have attempted to augment wing-lift beyond the capabilities of mechanical flaps, slots, and the like. Theoretical studies and wind tunnel tests promised large gains in aircraft performance, but flight installations all over the world proved a long series of failures. Because of the problems inherent in the operation of high-speed jet aircraft, the Department of Defense revived interest in lift-increase systems. A development of the Bureau of Aeronautics recently flight-tested on a Grumman jet fighter demonstrated what is considered the first practical, operationally suitable lift-augmentation system. Under the name of the BuAer Supercirculation System, whereby engine power was successfully diverted to create lift, it has provided new impetus for industry-wide research in the field.
Technical Paper
Wind and Temperature Database for Flight Planning
1981-10-01
811068
This paper discusses the importance of enroute wind conditions and the need for a wind measurement system which provides accurate and timely observations of wind and temperature conditions aloft. Recent advances in remote measurement of winds, temperature, and humidity such as the Stratospheric-Tropospheric radars and profilers developed at the National Oceanic and Atmospheric Administration’s Environmental Research Lab form the basis of such a system. A domestic system could and should be established using these devices together with a near real time winds aloft data dissemination network. Estimates of the saving in aircraft fuel consumption benefits range from 1 to 3 percent per year, or from $ 100 to $ 300 million for U.S. aviation system users at current prices and consumption.
