Twin Engine Helicopter Power Requirements
NORM herausgegeben am 1.6.1997
Bezeichnung normen: SAE AIR1850A
Ausgabedatum normen: 1.6.1997
Land: Amerikanische technische Norm
Kategorie: Technische Normen SAE
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