SAE AIR 1703A:2017-12-05

In-Flight Thrust Determination, SAE AIR1703 reviews the major aspects of processes that may be used for the determination of in-flight thrust (IFT). It includes 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. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide (Reference 1.1 ¹), which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed in this document, and these assumptions must be evaluated during the conduct of the program.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
Cancellation date	2017-12-05
Confirmation date	2017-12-05
ICS	49.050 : Aerospace engines and propulsion systems
Number of pages	316
Replace	SAE AIR 1703:2004-11-17
Replaced by	SAE AIR 1703A (2017-12-05)
Set	AEROPAKS10U-10
Year	2017
Document history	SAE AIR 1703:2004-11-17
Country	USA
Keyword	SAE 1703;SAE AIR1703A;SAE AIR1703A;SAE AIR 1703