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Universal series

ROS-RYB 182

Larger body (300 g) and a 0.123 MPa outlet: 1.82 L/min with 44.5 W nominal. Built for engines around 40 kg thrust where the 120/135 bodies run out of pressure.

Flow rate1.82 L/min
Outlet pressure0.123 MPa
Mass300 g

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0.123 MPa — highest of the 12 V line
44.5 W nominal, 29 936 r/min
300 g machined body

Engine class≤ 40 kg

Documents Datasheet · PDF 103 KB ↓

Typical applications

~40 kg thrust engines
Higher-pressure UAV fuel systems
Fuel-injection test benches

Technical data

Technical data
Mass	≤ 300 g
Motor poles	5 pairs (10 poles)
Supply voltage	12 ± 2 V DC
Current	3.72 A
Power	44.5 W rated · ≤ 70 W max
Speed at rated voltage	29 936 r/min
Outlet pressure	0.123 MPa
Flow rate	1.82 L/min
Continuous life	≥ 12 h
Cumulative life	≥ 100 h
Operating temperature	−40 … +70 °C
Altitude	0 – 8 000 m
Fuel	RP-3 jet fuel (≥ 70 %)
Leakage	No leakage at rated condition