Freezing Point of Aviation Fuels
ASTM D2386, DIN 51421, IP 16, ISO 3013
Freezing point of aviation fuels
Covers the determination of the temperature below which solid hydrocarbon crystals may form in aviation turbine fuels and aviation gasoline.
Art. LT/FP-237000/M
Manual Freezing Point - ASTM D2386
Double tube 30 × 240 mm fitted with cap with a stopper supporting the thermometer and moisture-proof collar through which the stirrer passes
Dewar jar 75 × 280 mm mount-based
Stirrer made of 1.6 mm brass rod bent into a smooth three-loop spiral at the bottom
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Freezing Point of Aviation Fuels
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Art. LT/FP-237500/M
Electric Freezing Point - ASTM D2386
Double tube 30 × 240 mm fitted with cap
Dewar jar 75 × 280 mm mount-based
Geared motor for stirring at 80 rpm with wire stirrer
PT100 sensor
Mounted on a plate structure painted with anti-acid epoxy products
Power supply 220 Vac 50/60 Hz
Power Supply
220Vac 50/60 Hz
Dimensions
cm 40 × 50 × 80
Weight
kg 10
Accessories
T-AS114C: thermometer ASTM 114C IP 14C
Spare Parts
LAB-102-371: double tube
LAB-102-372: wire stirrer
LAB-102-373: Dewar jar 75 × 280 mm
LAB-102-374: cap
LAB-102-375: PT100 sensor, only for LT/FP-237500/M
CE marked
