THE MEASUREMENT OF ENGINE THRUST IN AN ALTITUDE TEST FACILITY

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

02-14-2018

Publisher

SAE International

1. SCOPE
2. REFERENCES
3. DESCRIPTION OF ALTITUDE TEST FACILITY
4. TEST OPERATIONS
5. TECHNICAL DISCUSSION
6. NOTES
APPENDIX A - USE OF NON-SI (METRIC) UNITS

Specifies engine tests performed in Altitude Test Facilities (ATFs) with the primary purpose of determining steady state thrust at simulated altitude flight conditions as part of the in-flight thrust determination process.

Committee	E-33
DocumentType	Revision
Pages	50
PublisherName	SAE International
Status	Current
Supersedes	SAE AIR 5771 : 2015

SAE AIR 1703 : 2012	IN-FLIGHT THRUST DETERMINATION
SAE AIR 5450 : 2014	ADVANCED DUCTED PROPULSOR IN-FLIGHT THRUST DETERMINATION
ASME PTC19.1 : 2013	TEST UNCERTAINTY
SAE AIR 5925 : 2013	MEASUREMENT UNCERTAINTY APPLIED TO COST-EFFECTIVE TESTING
SAE AIR 1678 : 2016	UNCERTAINTY OF IN-FLIGHT THRUST DETERMINATION
ISO 2533:1975	Standard Atmosphere
SAE AS 755 : 2014	AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION