MAMMOTH

250 SE SERIES

The Jet Central turbines are in its own right a single stage centrifugal flow gas turbine engine, configured to operate as a Turbojet engine for use mainly, but not exclusively, in remotely piloted fixed wing aircraft. Such aircraft and their control systems must be appropriately designed and built to be compatible with the performance of the Turbojet engine.

CATEGORY

56.20 lbs thrust

SPECIFICATIONS

Thrust
Idle Thrust
RPM Range
Weight
Diameter
Length
Exhaust Gas Temperature
Fuel Consumption
250 Newtons (56.20 Lbs) @ 108,000 RPM
8 Newtons (1.8 Lbs) @ 28,000 RPM
28,000 – 108,000
2.28 Kg (5.02 Lbs)
124.1 mm (4.89”)
325.4mm (12.81”)
500º C – 700º C
0.81 Lt/min (28.51 Oz/min) @ 108 k
Thrust
250 Newtons (56.20 Lbs) @ 108,000 RPM
Idle Thrust
8 Newtons (1.8 Lbs) @ 28,000 RPM
RPM Range
28,000 – 108,000
Weight
2.28 Kg (5.02 Lbs)
Diameter
124.1 mm (4.89”)
Length
325.4mm (12.81”)
Exhaust Gas Temperature
500º C – 700º C
Fuel Consumption
0.81 Lt/min (28.51 Oz/min) @ 108 k

PERFORMANCE GRAPHS

Here you’ll find detailed technical specifications, including fuel consumption, pressure-thrust, operating temperature, and more. If your project requires additional data or customized information, our team will be happy to assist you. Simply use the contact form below, and we’ll get back to you promptly.

GET IN TOUCH

Please leave a message and we’ll contact you as soon as possible.