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Twin Engine Helicopter Power Requirements
- Aerospace Standard
- AIR1850A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
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Topic
Data Sets - Support Documents
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TABLE 2 |
Issuing Committee
S-12 Powered Lift Propulsion Committee
Provides guidance and standardization for the better utilization of helicopter powerplants through studies of current practices in engine design, engine/airframe interface, and engine operation.
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