High-Voltage Electrostatic Effect Test

High-Voltage Electrostatic Effect Test
Details:
This test system is used for: verification of high-voltage electrostatic effects during in-flight refueling (applicable to any aircraft refueling in flight), verification of high-voltage electrostatic effects during vertical lifting (applicable to helicopters and systems externally sling-on or transported by helicopters), and testing of high-voltage electrostatic effects during in-flight replenishment of ordnance.
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Description
Technical Parameters

Service Content

 

Package Name

Package Features

Test Standard

Test Qualification

High-Voltage Electrostatic Effect Test

- High-voltage electrostatic effect verification for aerial refueling (applicable to any aircraft performing in-flight refueling)- High-voltage electrostatic effect verification for vertical lifting (applicable to helicopters and systems externally suspended or transported by helicopters)- High-voltage electrostatic effect test for aerial supply of ordnance

- GJB 1389A-2005 System Electromagnetic Compatibility Requirements (Clauses 5.7.2, 5.7.4)- GJB 8848-2016 System Electromagnetic Environmental Effects Test Methods (Methods 701, 703)- GJB 573A-1998 Method 601 Electrostatic Discharge Test- MIL-STD-464A/B/C/D System Electromagnetic Compatibility Requirements (Clauses 5.7.2, 5.7.4)

CNAS Accreditation

 

Scope of Service


This product can provide high-voltage electrostatic discharge (ESD) testing.

 

Testing Standards


GJB 1389A-2005 System Electromagnetic Compatibility Requirements 5.7.2, 5.7.4
GJB 8848-2016 System Electromagnetic Environment Benefit Test Methods Method 701, Method 703
GJB 573A-1998 Method 601 Electrostatic Discharge Test
MIL-STD-464A/B/C/D System Electromagnetic Compatibility Requirements 5.7.2, 5.7.4

 

Test Items: High Voltage Electrostatic Effect Test; Discharge voltage continuously adjustable, maximum support ±350kV;

Charging capacitor: 1000pF;

Discharge resistance: maximum 1Ω;

Discharge inductance: maximum 20μH;

Charging voltage is controlled during testing.

Relevant Qualifications: CNAS;

Test Cycle: 5-7 working days.

 

Service Background

 

During flight, aircraft are subject to various charging factors, including electrostatic charging (several hundred kV can be charged within 1 second), atmospheric electric field induction charging, geomagnetic field induction charging, plasma charging (high-temperature, high-pressure jet engine exhaust negatively charges the aircraft), and strong field irradiation. Since grounding is not possible during flight, the electrostatic voltage of the aircraft can reach 300kV. When the aircraft comes into contact with external objects, it will generate a huge spark discharge (e.g., between the refueling nozzle and the refueling port, between the helicopter hook and the load, between unloading cargo and the ground), which can lead to a reduction or damage to the system performance, or even cause safety accidents.

 

Our Advantages


GRGTEST is a nationally recognized professional third-party testing organization, providing one-stop services;
GRGTEST EMC Testing Center has established 8 laboratories nationwide, possessing a professional multidisciplinary expert team and advanced testing equipment;
GRGTEST EMC laboratories hold CMA and CNAS accreditations, implement a nationwide integrated management model, and actively participate in various proficiency testing projects to ensure that test results are impartial, accurate, and traceable.

 

 

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