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MIL-STD-704 Aircraft Electric Power CharacteristicsThis standard establishes the requirements and characteristics of aircraft electric power provided at the input terminals of electric utilization equipment. MIL-HDBK-704-1 through-8 defines test methods and procedures for determining airborne utilization equipment compliance with the electric power characteristics requirements defined herein. Electromagnetic interference and voltage spikes are not covered by this standard.

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MIL-STD-704F


430


425

Maximum Limit



420


410


407


400


Minimum Limit


393


390


380




375

Note:

1. Steady state limits do not include the distrubances allowed in Table I.



370


0           1           2           3           4           5           6           7           8           9           10          11         12         13         14


Time from Onset of Transient (seconds)



FIGURE 5.  Envelope of normal 400 Hz AC frequency transient.


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