An Overview of MIL-STD-704, MIL-HDBK-704, 28 Volt DC Aircraft Utilization Compliance Testing, Electrical Power Quality Causes and Impacts 2004-01-3156
Aircraft electrical power quality effects the operation and life of avionics equipment. The military interface document that defines aircraft electrical power at the input to utilization equipment is MIL-STD-704. Testing is required to demonstrate compatibility of avionics with aircraft electrical power. This paper summarizes the aircraft electrical operating conditions and power groups of MIL-STD-704. The paper also gives an overview of the test guidance for 28 volt DC aircraft utilization equipment provided in the recently published handbook MIL-HDBK-704, “Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics”. Common causes of power quality parameters and the effects on avionics are given.
Citation: Burdette, A., Goodnow, M., and Singer, C., "An Overview of MIL-STD-704, MIL-HDBK-704, 28 Volt DC Aircraft Utilization Compliance Testing, Electrical Power Quality Causes and Impacts," SAE Technical Paper 2004-01-3156, 2004, https://doi.org/10.4271/2004-01-3156. Download Citation
Author(s):
Arthur Burdette, Michael Goodnow, Charles Singer
Affiliated:
Anteon Corporation, Naval Air Systems Command, Patuxent River Maryland
Pages: 10
Event:
Power Systems Conference
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 2004 Transactions Journal of Aerospace-V113-1
Related Topics:
Electric power
Aircraft
Test procedures
Technical review
Tools and equipment
Avionics
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