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Razdan, RahulKhalighi, YaserKhalkhali, MohsenAlonso da Silva, Fabio
Fang, ChenRazdan, rahulBeiker, SvenTaleb-Bendiab, Amine
Beiker, SvenBock, ThomasTaiber, Joachim
Beiker, SvenMuelaner, Jody E.Razdan, Rahul
Beiker, SvenPorcel Magnusson, CristinaWaraniak, John
Coyner, KelleyBittner, JasonLambermont, SergeDe Boer, Niels
Lehmann, JohannesMoorehead, StewartMuelaner, Jody E.
Abdul Hamid, Umar ZakirRoth, ChristianNickerson, JeffreyLyytinen, KalleKing, John Leslie
This AS provides the minimum performance requirements for the following types of inflatable emergency evacuation devices (hereinafter referred to as device[s]): 1 Type I - Inflatable Slide: A device suitable for assisting occupants in descending from a floor-level airplane exit or from an airplane wing to the ground. A Type I off-wing slide is a device that does not include a ramp. 2 Type II - Inflatable Slide/Raft: A device suitable for assisting occupants in descending from a floor-level airplane exit or an airplane wing to the ground that is also designed to be used as a life raft. A Type II off-wing slide/raft is a device that does not include a ramp. 3 Type III - Inflatable Exit Ramp: A device suitable for assisting occupants in descending from certain overwing exits to an airplane wing. 4 Type IV - Inflatable Ramp/Slide: A device suitable for assisting occupants from an overwing exit or airplane wing to the ground. It is a combination ramp and wing-to-ground device. 5 Type VS-9A Safety Equipment and Survival Systems Committee
This specification establishes the requirements for flake or granular cetyl alcohol, solvents for dissolving the cetyl alcohol, preparation and application requirements for use of cetyl alcohol as an installation lubricant on mechanical fasteners, such as pins, bolts, nuts, washers, threaded or nonthreaded fastening devices, and inspection criteria for coated partsE-25 General Standards for Aerospace and Propulsion Systems
This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.5AMS D Nonferrous Alloys Committee
This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 square inches (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.5AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stockAMS F Corrosion and Heat Resistant Alloys Committee
This specification covers unalloyed copper in the form of sheet, strip, and plate at least 0.015 inch (0.38 mm) in nominal thicknessAMS D Nonferrous Alloys Committee
This SAE Aerospace Information Report (AIR) describes the Architecture Framework for Unmanned Systems (AFUS). AFUS comprises a Conceptual View, a Capabilities View, and an Interoperability View. The Conceptual View provides definitions and background for key terms and concepts used in the unmanned systems domain. The Capabilities View uses terms and concepts from the Conceptual View to describe capabilities of unmanned systems and of other entities in the unmanned systems domain. The Interoperability View provides guidance on how to design and develop systems in a way that supports interoperabilityAS-4JAUS Joint Architecture for Unmanned Systems Committee