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Safety Considerations for Lasers Projected in the Navigable Airspace

G10T Laser Safety Hazards Committee
  • Aerospace Standard
  • ARP5293A
  • Current
Published 2020-03-10 by SAE International in United States
This document applies to laser proponents involved with the use of laser systems outdoors. It may be used in conjunction with AS4970, ARP5535, and ARP5572 and the ANSI Z136 series of laser safety standards.
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Attack Reconnaissance Helicopter

  • Magazine Article
  • TBMG-36063
Published 2020-02-01 by Tech Briefs Media Group in United States

Bell Textron Inc Fort Worth, TX +1 817-280-2011

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Aerospace & Defense Technology: February 2020

  • Magazine Issue
  • 20AERP02
Published 2020-01-30 by SAE International in United States
Rad-Hard Microelectronics for Space ApplicationsOutsourcing Plasma Treatments for Surface ModificationAdding Context to Full-Motion Video for Improved Surveillance and Situational AwarenessImplementing an Aerospace Factory of the Future90° Hybrid Coupled Power Amplifier - Pros and ConsA New Network Design for the "Internet from Space"Future Advances in Electronic Materials and Processes - Flexible Hybrid Electronics Despite progress being made, there are still significant obstacles to the manufacture and use of flexi-ble hybrid electronics in military applications.Heterogeneous Integration Technology Integrating different types of devices and materials could increase their functional density, improving the performance of electro-optic systems for sensor applications.The Impact of Cyber Cameras on the Intelligence Community The ability to covertly access and manipulate cyber cameras could provide valuable strategic data for the US intelligence community.Calculating Electrical Requirements for Direct Current Electric Actuators When designing electro-mechanically actuated systems, there are several electrical design requirements that must be determined.Weyl Semimetals (WSM) for Electronics Applications New synthesized materials open the way to govern the density of helicity, axial charge, and its flow, axial current.Energy Harvesting for Soft-Matter Machines and Electronics…
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Coupling Assembly, Hydraulic Self Sealing, Quick Disconnect

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS1709B
  • Current
Published 2020-01-06 by SAE International in United States
This specification covers the requirements for aircraft, hydraulic, self-sealing, quick disconnect couplings, for use in Type II hydraulic systems (-65 to +275 °F temperature range) as defined by AS5440.
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Specification Guide for Power Drive Units (PDUs)

A-6B3 Electro-Mechanical Actuation Committee
  • Aerospace Standard
  • ARP5384
  • Current
Published 2020-01-06 by SAE International in United States
This Recommended Practice provides a guide for specifying general design, performance, and test requirements for power drive units (PDUs) for flight controls and other applications.
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Predicting Photometric Degradation of Exterior Aircraft Lights

A-20B Exterior Lighting Committee
  • Aerospace Standard
  • ARP6621
  • Current
Published 2019-12-09 by SAE International in United States
This Aerospace Recommended Practice provides guidance for designers and specifiers of aircraft exterior lighting. Typical causes of light degradation and methods of predicting performance degradation in the aircraft environment are given. Although the document considers only exterior lighting, many of the principles and methods discussed apply to interior or flight deck lighting as well.
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Aircraft Fuel System Design Guidelines

AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
  • Aerospace Standard
  • AIR7975
  • Current
Published 2019-12-05 by SAE International in United States
This document describes the major design drivers and considerations when designing a fuel system for a large commercial aircraft. It discusses the design at a system/aircraft level, and is not intended as a design manual for individual system components, though it does refer out to other SAE specifications where more detail on specific components and sub-systems is given. It does include examples of a number of calculations associated with sizing of fuel systems, based on those given in NAV-AIR-06-5-504, as well as an appendix summarizing basic fluid mechanical equations which are key for fuel system design. It is acknowledged that most of these calculations would today be performed by modelling tools, rather than by hand, but it is considered important for the designer to understand the principles. It is intended that later issues of this document will include appendices which give specific considerations for military aircraft, smaller commercial aircraft, and rotorcraft.
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Technology Impact Forecasting for Multi-Functional Composites

  • Magazine Article
  • TBMG-35679
Published 2019-12-01 by Tech Briefs Media Group in United States

To survive within today's stringent economic environment, aircraft design, particularly military aircraft design, has been experiencing a paradigm shift from an emphasis on design for optimum performance to design for system effectiveness. As a consequence, designers and manufacturers are increasingly considering the addition of new technologies to aircraft design to reduce their cost, increase their operating capacities, and optimize new capabilities.

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Technology Impact Forecasting for Multi-Functional Composites

Aerospace & Defense Technology: December 2019

  • Magazine Article
  • 19AERP12_09
Published 2019-12-01 by SAE International in United States

Multi-functional composites offer a possible solution to the conflicting design goals of making new aircraft lighter, stronger, faster, and more environmentally sustainable.

To survive within today's stringent economic environment, aircraft design, particularly military aircraft design, has been experiencing a paradigm shift from an emphasis on design for optimum performance to design for system effectiveness. As a consequence, designers and manufacturers are increasingly considering the addition of new technologies to aircraft design to reduce their cost, increase their operating capacities, and optimize new capabilities.

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Paint System, Fluorescent, Removable, for Aircraft Application

AMS G8 Aerospace Organic Coatings Committee
  • Aerospace Material Specification
  • AMSP21600B
  • Current
Published 2019-10-28 by SAE International in United States
This specification establishes the requirements for a high visibility, durable, exterior fluorescent coating system consisting of a pigmented fluorescent coating with a clear protective overcoat containing a weathering stabilizer. This coating system is capable of being removed without softening the permanent undercoats.
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