SAE AIR 5771 : 2018
Current
The latest, up-to-date edition.
THE MEASUREMENT OF ENGINE THRUST IN AN ALTITUDE TEST FACILITY
Hardcopy , PDF
English
14-02-2018
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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 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 |
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