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Header Tank Fuel Sensor

TECHNICAL SPECIFICATION

Product specifications

Repeatability 2.54 mm (0.1 in)
Response time 200 ms
Input voltage 5 – 24 VDC
Leakage current Less than 50 μA
Output TTL (high) – Low Fuel Level

Wiring

RED 5 – 24 VDC input
BLACK Common (Ground)
WHITE TTL Output

Environmental Specifications

Electronic component sealing IP68
MIL-STD 810F, 512.4
Electronic operating temperature range -40°C to +125°C
Immersed probe operating temperature range -40°C to +150°C
Storage temperature range -40°C to +150°C
Humidity Designed to meet the requirements of SAE J1455
Vibration Design guideline used: SAE J1455 & SAE J1241
15g RMS 24 – 2000Hz
EMC RE 102, RF103 200V/M

Sensor Mounting

The sensor is located so that the low fuel condition occurs at approximately 40% of the header tank volume. The sensor can be relocated by the user in order to change the position of the measurement.

When the header tank fuel level sensor indicates low fuel condition, it is essential to land the UAV immediately.

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