Twin Engine Helicopter Power Requirements
NORMA vydaná dňa 1.6.1997
Označenie normy: SAE AIR1850A
Dátum vydania normy: 1.6.1997
Krajina: Americká technická norma
Kategória: Technické normy 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