Procedure is applicable to aircraft motors which operate from constant-frequency, nominally 400-cycle-per-second, constantvoltage, (nominally 115 volt line to neutral, 3-phase four-wire or 115 volt single-phase) alternating-current aircraft power systems. This aircraft power system is defined by paragraph 3.2.1.3, Type I of Military Specification No. MIL-E-7894. The test methods described herein will be suitable for test of machines of different frequency and voltage ranges. However, test equipment must be chosen suitable for the desired ranges
- Status
- Inactive-Withdrawn Standard
- History
-
- Published:
- 1959-12-31
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