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CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS
Translate name
STANDARD published on 1.1.2020
Designation standards: SAE AIR1296
Publication date standards: 1.1.2020
SKU: NS-983261
Country: American technical standard
Category: Technical standards SAE
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.
SUBJECT TAXONOMY: Hybrid engines, Turboprop engines, Rotary-wing aircraft
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
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