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Society of Allied Weight Engineers, Inc.
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Home / SAWE Technical Papers / Page 99

SAWE Technical Papers

Showing 1569–1584 of 2092 resultsSorted by latest

  • 713. Metrication - Implementation to the Metric (SI) System in the United Kingdom

    713. Metrication – Implementation to the Metric (SI) System in the United Kingdom

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  • 712. Recent Developments in the Trend Toward Use of SI Units

    712. Recent Developments in the Trend Toward Use of SI Units

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  • 710. Introduction to the Metric Session

    710. Introduction to the Metric Session

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  • 705. Concorde

    705. Concorde

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  • 703. Justification of Measurement System Cost

    703. Justification of Measurement System Cost

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  • 702. Aerospace Vehicle Costs Based on Weights

    702. Aerospace Vehicle Costs Based on Weights

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  • 700. Utilization of the IBM 360 for Mass Properties Accounting

    700. Utilization of the IBM 360 for Mass Properties Accounting

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  • 697. Electroluminescent Lighting as Used in Aviation Applications

    697. Electroluminescent Lighting as Used in Aviation Applications

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  • 696. Weight Control of Finished Parts by Dynamic Etching

    696. Weight Control of Finished Parts by Dynamic Etching

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  • 695. Beryllium Technology and Application

    695. Beryllium Technology and Application

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  • 694. Mass Properties Uncertainty Analysis of Aerospace Vehicle Hardware

    694. Mass Properties Uncertainty Analysis of Aerospace Vehicle Hardware

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  • 693. Titan III Propellant Management Technique

    693. Titan III Propellant Management Technique

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  • 691. Confidence Problems in Performance Prediction

    691. Confidence Problems in Performance Prediction

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  • 688. Weight Growth - A Philosophy

    688. Weight Growth – A Philosophy

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  • 687. The Contribution of an Inadequate Allowance for Non-Optimum Factors to Weight Growth

    687. The Contribution of an Inadequate Allowance for Non-Optimum Factors to Weight Growth

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  • 686. Hypothesis on Weight Growth During the Development Stage of Aircraft

    686. Hypothesis on Weight Growth During the Development Stage of Aircraft

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