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SAE AIR1296

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Concurrent Design of Engines and Specifications of Starting Systems for Helicopters

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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.

SDO SAE: SAE International
Document Number AIR1296
Publication Date Oct. 1, 1975
Language en - English
Page Count 1
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Oct. 1, 1975 AIR1296 Revision