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This specification covers a corrosion and heat-resistant steel in the form of welded tubing.

This specification covers a corrosion and heat resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings over 0.50 inch (12.7 mm) in nominal diameter or least distance between parallel sides (see 8.6).

This SAE Aerospace Standard (AS) specifies minimum performance standards for all types of electronic displays and electronic display systems that are intended for use in the flight deck by the flight crew in all 14 CFR Part 23, 25, 27, and 29 aircraft. The requirements and recommendations in this document are intended to apply to all installed electronic displays and electronic display systems including those that have a touch screen interface within the flight deck, regardless of intended function, criticality, or location within the flight deck, but may also be used for non-installed electronic displays. This document provides baseline requirements and recommendations (see 2.3 for definitions of “shall” and “should”). This document primarily addresses hardware requirements, such as electrical, mechanical, optical, and environmental. It does not address system specific functions.

This specification covers two types of free-machining, corrosion and heat-resistant steel in the form of bars, wire, forgings, and forging stock.

Ceramic matrix composite (CMC) use is up across the aerospace market, and among the fastest-growing trends in the global aviation industry. CMC material and component use in aircraft engines, specifically, is projected to double over the next five years, according to a new report from analysts at Stratview Research in Telibandha, India.

Autonomous Driving Software needs a rethink

Multi-energy platforms will need to accommodate both combustion-engine and electrified propulsion systems.

2019 Jaguar I-Pace brings benchmark dynamics to electrified segment

General Motors, BMW, Sika Automotive, U.S. Steel, AAM, Asahi Kasei and Mazda recognized for their lightweighting achievements at the Management Briefing Seminars.

This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of sand castings.

This specification covers an aluminum alloy in the form of hand forgings up to 8 inches, incl (203 mm, incl) in nominal thickness, and rolled rings up to 3.5 inches, incl (89 mm, incl) in nominal thickness (see 8.5).

Abstract The advancement towards development of autonomy follows either the bottom-up approach of gradually improving and expanding existing Advanced Driver Assist Systems (ADAS) technology where the driver is present in the control loop or the top-down approach of directly developing autonomous vehicle hardware and software using alternative approaches without the driver present in the control loop. Most ADAS systems today fall under the classification of SAE Level 1 which is also referred to as the driver assistance level. The progression from SAE Level 1 to SAE Level 2 or partial automation involves the critical task of merging automated lateral control and automated longitudinal control such that the tasks of steering and acceleration/deceleration are not required to be handled by the driver under certain conditions [1].

This document covers oil transport mechanisms from the power cylinder system which might affect oil consumption. It will not discuss in detail the oil consumption mechanisms from other systems or engine components.

This document describes the major techniques for measuring oil consumption. It does not cover all the sub-variations that might be used to make this measurement.

This specification covers a titanium alloy in the form of sheet, strip, and plate on product 0.008 to 3.000 inches (0.20 to 76.20 mm), inclusive in thickness.

This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (see 8.4).

This specification covers a corrosion resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (see 8.4).

This specification covers the requirements for electrodeposited silver on other metals, usually with a nickel strike between the basis metal and the silver.

Today, L3 WESCAM delivered the first of its first MX-15 electro-optical and infrared system to Airbus Defense and Space in support of Canada’s Fixed-Wing Search and Rescue aircraft replacement program.

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.