AIR1296: CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS - Information Report

Features

Issuing Committee: S-12 Powered Lift Propulsion Committee

Scope

Content: It is recommended that all helicopter engine development programs include an evaluation of engine starting requirements. The evaluation should include starting requirement effects on helicopter weight, cost, and mission effectiveness. The evaluation should be appropriate to the engine stage of development.

Meta Tags

Topics: Aircraft propulsion systems
Helicopters
Starters and starting
Engines
Design processes

Details

DOI: https://doi.org/10.4271/AIR1296

Pages: 1

Citation: SAE International Information Report, CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS, SAE Standard AIR1296, Reaffirmed January 2020, Issued October 1975, https://doi.org/10.4271/AIR1296.

Additional Details

Publisher: SAE International

Published: Jan 31, 2020

Product Code: AIR1296

Content Type: Information Report

Status: Reaffirmed

Language: English