Twin Engine Helicopter Power Requirements
NORMA vydána dne 1.6.1997
Označení normy: SAE AIR1850A
Datum vydání normy: 1.6.1997
Země: Americká technická norma
Kategorie: 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