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Twin Engine Helicopter Power Requirements
STANDARD published on 1.6.1997
Designation standards: SAE AIR1850A
Publication date standards: 1.6.1997
SKU: NS-477184
Country: American technical standard
Category: Technical standards 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
Latest update: 2024-09-08 (Number of items: 2 346 102)
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