SAE AIR 5771A:2018-02-14

This report covers 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. As such it is complementary to AIR1703 and AIR5450, published by the SAE E-33 Technical Committee. The gross thrust determined using such tests may be used to generate other thrust-related parameters that are frequently applied in the assessment of propulsion system performance. For example: net thrust, specific thrust, and exhaust nozzle coefficients.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
ICS	49.050 : Aerospace engines and propulsion systems
Number of pages	50
Replace	SAE AIR 5771:2015-09-14
Set	AEROPAKS10U-10
Year	2018
Document history	SAE AIR 5771:2015-09-14
Country	USA
Keyword	SAE 5771;SAE AIR5771A;SAE AIR5771A;SAE AIR 5771