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SAE AIR 1703 : 2012

SAE AIR 1703 : 2012

IN-FLIGHT THRUST DETERMINATION

SAE International

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Table of Contents

1. SCOPE
2. REFERENCES
3. PROGRAM PLANNING GUIDELINES
4. DEFINITIONS AND METHODOLOGY
5. PROPULSION SYSTEM INSTALLATIONS
6. IN-FLIGHT THRUST METHODS
7. CALIBRATION TECHNIQUES
8. TEST DATA ACQUISITION SYSTEMS
9. ANALYSIS AND VALIDATION OF THRUST DETERMINATION
10. NOTES
APPENDIX A - COMMITTEE E-33 HISTORY
APPENDIX B - BIBLIOGRAPHY
APPENDIX C - THRUST AND DRAG ACCOUNTING
APPENDIX D - BACKGROUND FOR THRUST/DRAG BOOKKEEPING
APPENDIX E - CASE STUDIES AND APPLICATIONS

Abstract

Specifies the major aspects of processes that may be used for the determination of in-flight thrust (IFT). It also covers discussions of basic definitions, analytical and ground test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee E-33

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