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SAE AIR6064

Reverse Thrust
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SAE AIR6064

Reverse Thrust

PUBLISH DATE 2018
PAGES 69
SAE AIR6064
Propulsion measurements and thrust methods presented in the current published versions of AIR1703 and AIR5450 place a primary focus on the engine reactionary force (thrust) acting to propel an aircraft in the forward direction. In contrast, this document addresses the use of the engine reactionary force in the opposite direction (reverse thrust) to supplement aircraft deceleration. This document’s application spans commercial and military transport turbofan engine applications for various engine and reverse thrust configurations. The discussion and examples primarily focus on separate flow exhaust turbofan engines. Piston and turboprop variable-pitch propeller blade applications are not covered. Although reverse thrust has been utilized for in-flight deceleration, primarily for short takeoff and landing aircraft and military fighter applications, this application of reverse thrust is only covered in a cursory manner.
SDO SAE: SAE International
Document Number AIR6064
Publication Date May 7, 2018
Language en - English
Page Count 69
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
May 7, 2018 AIR6064 Revision