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SAE AIR1850A

Twin Engine Helicopter Power Requirements

STANDARD published on 1.6.1997

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The information about the standard:

Designation standards: SAE AIR1850A
Publication date standards: 1.6.1997
Country: American technical standard
Category: Technical standards SAE

Annotation of standard text SAE AIR1850A :


This SAE Aerospace Information Report (AIR) defines the power spectrum during normal and emergency operations of a twin engine helicopter and thereby postulates suitable power plant rating structures. This document does not address the power requirements for single engine helicopters or those with more than two engines.

SUBJECT TAXONOMY: Hybrid engines, Turboprop engines, Rotary-wing aircraft
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard