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SAE AIR 1602:1991-05-01
STARTER SYSTEM OPTIMIZATION START ANALYSIS, TURBINE ENGINE - ELECTRIC, BATTERY POWERMore info
This SAE Aerospace Information Report includes procedures for the analysis of a gas turbine engine start. It utilizes a standard form for the essential starting characteristics of the gas turbine engine and for the starting power capability of the aircraft battery. This report illustrates the format of the characteristic which is provided by the electric starter to transform the battery electric power (voltage and current) to the mechanical power (torque and speed) required to successfully start the engine.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 1991-05-01 |
| ICS | 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 12 |
| Set | AEROPAKS10U-10 |
| Year | 1990 |
| Document history | |
| Country | USA |
| Keyword | SAE 1602;SAE AIR1602;SAE AIR1602;SAE AIR 1602 |