CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS
NORMA vydána dne 1.1.2020
Označení normy: SAE AIR1296
Datum vydání normy: 1.1.2020
Země: Americká technická norma
Kategorie: Technické normy 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