SAE AIR 1850A:1997

$25.35

Twin Engine Helicopter Power Requirements

Published By	Publication Date	Number of Pages
SAE	1997-06-01	8

Guaranteed Safe Checkout

Categories: 49 - Aircraft and space vehicle engineering, SAE

If you have any questions, feel free to reach out to our online customer service team by clicking on the bottom right corner. We’re here to assist you 24/7.
Email:[email protected]

Description

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.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	1997-06-01
Pages Count	8
Language	English
Descriptors	Aircraft; Helicopters; Entry, descent, and landing; Fuel consumption; Hazards and emergency operations; Suppliers
File Size	30.7 KB
ICS Codes	49 - Aircraft and space vehicle engineering

Preview PDF


PDF Format	Searchable	Printable	Preview Now

SAE AIR 1850A:1997

Related products