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A 'STEP' Forward for Product Lifecycle Management

  • Magazine Article
  • TBMG-35365
Published 2019-10-01 by Tech Briefs Media Group in United States

The existence of countless proprietary file formats and the exchange of 3D CAD data has been a significant problem since the beginning of 3D CAD modeling. CAD applications and methods using digital data are constantly changing, which predicates the need for a solution to share validated and accurately translated data. Thus the birth of STEP242.

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A “STEP” Forward for Product Lifecycle Management

Aerospace & Defense Technology: October 2019

  • Magazine Article
  • 19AERP10_02
Published 2019-10-01 by SAE International in United States

The existence of countless proprietary file formats and the exchange of 3D CAD data has been a significant problem since the beginning of 3D CAD modeling. CAD applications and methods using digital data are constantly changing, which predicates the need for a solution to share validated and accurately translated data. Thus the birth of STEP242.

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Reliability Program Handbook

G-41 Reliability
  • Aerospace Standard
  • TAHB0009A
  • Current
Published 2019-05-03 by SAE International in United States
This Handbook provides “how to” guidance to industry and government for the reliability Activities and Methods contained in GEIASTD0009 for developing reliable products and systems, successfully demonstrating them during test and evaluation, and sustaining them throughout the system/product life cycle. GEIASTD0009 requires the developers and customer/users working as a team to plan and implement a reliability program that provides systems/products that satisfy the user’s requirements and expectations using a systems engineering approach. The four Objectives of GEIASTD0009 are listed below: Objective 1: Understand customer/user requirements and constraints. The team (developer, customer, and user) includes the Activities necessary to ensure that the user’s requirements and product needs are fully understood and defined, so that a comprehensive design specification and Reliability program plan are generated. Objective 2: Design and redesign for reliability. The developer implements a set of engineering Activities so that the resulting system/product satisfies the customer’s documented requirements and needs. Objective 3: Produce reliable systems/products. The developer performs the Activities that assure the customer that the reliability requirements and product needs have been satisfied. Objective…
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Standard Practice for Human Systems Integration

G-45 Human Systems Integration
  • Aerospace Standard
  • SAE6906
  • Current
Published 2019-02-08 by SAE International in United States
This Human Systems Integration (HSI) Standard Practice identifies the Department of Defense (DoD) approach to conducting HSI programs as part of procurement activities. This Standard covers HSI processes throughout design, development, test, production, use, and disposal. Depending on contract phase and/or complexity of the program, tailoring should be applied. The scope of this standard includes prime and subcontractor HSI activities; it does not include Government HSI activities, which are covered in the DoD HSI Handbook. HSI programs should use the latest version of standards and handbooks listed below, unless a particular revision is specifically cited in the contract.
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Standard Best Practices for System Safety Program Development and Execution

G-48 System Safety
  • Aerospace Standard
  • GEIASTD0010A
  • Current
Published 2018-10-18 by SAE International in United States
This document outlines a standard practice for conducting system safety. In some cases, these principles may be captured in other standards that apply to specific commodities such as commercial aircraft and automobiles. For example, those manufacturers that produce commercial aircraft should use SAE ARP4754 or SAE ARP4761 (see Section 2 below) to meet FAA or other regulatory agency system safety-related requirements. The system safety practice as defined herein provides a consistent means of evaluating identified risks. Mishap risk should be identified, evaluated, and mitigated to a level as low as reasonably practicable. The mishap risk should be accepted by the appropriate authority and comply with federal (and state, where applicable) laws and regulations, executive orders, treaties, and agreements. Program trade studies associated with mitigating mishap risk should consider total life cycle cost in any decision. This document is intended for use as one of the elements of project solicitation for complex systems requiring a systematic evaluation of hazards and mitigating measures. The Managing Authority may identify, in the solicitation and system specification, specific system safety…
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Modeling and Simulation Capabilities for Aerospace WDM LAN Applications

AS-3 Fiber Optics and Applied Photonics Committee
  • Aerospace Standard
  • AIR6006
  • Current
Published 2018-01-23 by SAE International in United States
This document provides an overview of currently available and need to be developed modeling and simulation capabilities required for implementing robust and reliable Aerospace WDM LAN applications.
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Maintenance Life Cycle Cost Model

AMS CACRC Commercial Aircraft Composite Repair Committee
  • Aerospace Standard
  • AIR5416
  • Current
Published 2016-10-13 by SAE International in United States
This document describes a life cycle cost model for commercial aircraft composite structure. The term life cycle cost used herein, refers to the airline costs for maintenance, spares support, fuel, repair material and labor associated with composites after introduction into service and throughout its useful life. This document contains the equations that can be programmed into software which is used to estimate the total cost of ownership aircraft, including structure. Modification costs and operating costs are estimated over a specified life (any period up to 30 years). Modification costs include spares holding, training, support equipment, and other system related costs. Annual operating costs include: Schedule interruption, fuel, spares, insurance, and maintenance. Maintenance costs are separated by scheduled maintenance or unscheduled damage, or can by grouped into the typical organizations of line, shop, and hangar maintenance. This Lifecycle Cost allows users to evaluate the impact of Service Bulletins, potential design changes, changes in maintenance programs, or effectiveness of maintenance operations.
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Configuration Management Standard Implementation Guide

G-33 Configuration Management
  • Aerospace Standard
  • GEIAHB649A
  • Current
Published 2016-03-01 by SAE International in United States
This handbook is intended to assist the user to understand the ANSI/EIA-649B standard principles and functions for Configuration Management (CM) and how to plan and implement effective CM. It provides CM implementation guidance for all users (CM professionals and practitioners within the commercial and industry communities, DoD, military service commands, and government activities (e.g., National Aeronautics and Space Administration (NASA), North Atlantic Treaty Organization (NATO)) with a variety of techniques and examples. Information about interfacing with other management systems and processes are included to ensure the principles and functions are applied in each phase of the life cycle for all product categories.
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MMLV: Life Cycle Assessment

Ford Motor Company-David Wagner
Life Cycle Assessment Consulting-Lindita Bushi
Published 2015-04-14 by SAE International in United States
The Multi Material Lightweight Vehicle (MMLV) developed by Magna International and Ford Motor Company is a result of a US Department of Energy project DE-EE0005574. The project demonstrates the lightweighting potential of a five passenger sedan, while maintaining vehicle performance and occupant safety. Prototype vehicles were manufactured and limited full vehicle testing was conducted. The Mach-I vehicle design, comprised of commercially available materials and production processes, achieved a 364kg (23.5%) full vehicle mass reduction, enabling the application of a 1.0-liter three-cylinder engine resulting in a significant environmental benefit and fuel reduction.The Regulation requirements such as the 2020 CAFE (Corporate Average Fuel Economy) standard, growing public demand, and increased fuel prices are pushing auto manufacturers worldwide to increase fuel economy through incorporation of lightweight materials in newly-designed vehicle structures. This paper is aimed at communicating the results of a life cycle assessment (LCA) study which compares the lightweight auto parts of the new multi material lightweight (MMLV) Mach-I (1.0l I3) vehicle design to the conventional auto parts of the baseline 2013 Ford Fusion (1.6l I4), both…
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The Next Generation of Systems Engineering: A Report by the GEIA G-47 Systems Engineering Panel

Systems Management Council
  • Aerospace Standard
  • GEIASE0001
  • Current
Published 2014-10-01 by SAE International in United States
No Abstract Available.
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