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Engines

  • GTM 85
  • GTM 100
  • GTM 140
  • GTM 160
  • GTM 180

Engine GTM 85

85N static thrust engine with or without equipment. Automatic start with liquid fuel (internal "kerostart"). Thermal protection of the turbine bearing by using an aluminum-steel shaft sleeve. The latest bearing lubrication system with directional air flow. A mounting bracket is supplied with the engine. The version with equipment has a microprocessor-based control module, interface for programming and parameter reading, fuel pump, starting and main fuel solenoid valves, electric and fuel lines. The product is intended for modeling applications. Requires careful reading of the safe use instructions. It may be a serious threat to health and life if used improperly.

with equipment:

6900zł

|

without equipment:

5700zł

Parameters

Static thrust: 85N

Rotor speed at max power: 120 000rpm

Minimum rotor speed: 33,000 rpm

Fuel consumption: 310 g/min

  • Supply: JET A1 + 3-5% MOBIL Jet Oil II, AEROSHELL 500/560
  • Automatic start "kerostart"
  • Built-in starter
  • Internal EGT sensor
  • Ignition from the internal spark plug
  • Optical rotation measurement

Dimensions: length 305mm diameter 110mm​

Weight of the whole set (engine + equipment): 1630g

 

  • Amplifier board with RPM and EGT sensors. Mounted on the engine.
  • Engine management and control module ProJET model HORNET III or newer. (ECU)
  • LCD panel for operating and programming turbine parameters. (GSU)
  • Fuel gear pump with 4mm pipe terminals.
  • Main and starting fuel valves.
  • A set of 4mm hydraulic pipes.
  • A set of electrical wires
  • MPX plug with adapter plate for battery connection.

 

Engine GTM 100

100N static thrust engine with or without equipment. Automatic start with liquid fuel (internal "kerostart"). Thermal protection of the turbine bearing by using an aluminum-steel shaft sleeve. The latest bearing lubrication system with directional air flow. A mounting bracket is supplied with the engine. The version with equipment has a microprocessor-based control module, interface for programming and parameter reading, fuel pump, starting and main fuel solenoid valves, electric and fuel lines. The product is intended for modeling applications. Requires careful reading of the safe use instructions. It may be a serious threat to health and life if used improperly.

with equipment:

7600zł

|

without equipment:

6400zł

Parameters

Static thrust: 100N

Rotor speed at max power: 120 000rpm

Minimum rotor speed: 33,000 rpm

Fuel consumption: 320 g/min

  • Supply: JET A1 + 3-5% MOBIL Jet Oil II, AEROSHELL 500/560
  • Automatic start "kerostart"
  • Built-in starter
  • Internal EGT sensor
  • Ignition from the internal spark plug
  • Optical rotation measurement

Dimensions: length 305mm diameter 110mm​

Weight of the whole set (engine + equipment): 1680g

 

  • Amplifier board with RPM and EGT sensors. Mounted on the engine.
  • Engine management and control module ProJET model HORNET III or newer. (ECU)
  • LCD panel for operating and programming turbine parameters. (GSU)
  • Fuel gear pump with 4mm pipe terminals.
  • Main and starting fuel valves.
  • A set of 4mm hydraulic pipes.
  • A set of electrical wires
  • MPX plug with adapter plate for battery connection.

 

 

Engine GTM 140

140N static thrust engine with or without equipment. Automatic start with liquid fuel (internal "kerostart"). Thermal protection of the turbine bearing by using an aluminum-steel shaft sleeve. The latest bearing lubrication system with directional air flow. A mounting bracket is supplied with the engine. The version with equipment has a microprocessor-based control module, interface for programming and parameter reading, fuel pump, starting and main fuel solenoid valves, electric and fuel lines. The product is intended for modeling applications. Requires careful reading of the safe use instructions. It may be a serious threat to health and life if used improperly.

with equipment:

8700zł

|

without equipment:

7300zł

Parameters

Static thrust: 140N

Rotor speed at max power: 120 000rpm

Minimum rotor speed: 33,000 rpm

Fuel consumption: 360 g/min

  • Supply: JET A1 + 3-5% MOBIL Jet Oil II, AEROSHELL 500/560
  • Automatic start "kerostart"
  • Built-in starter
  • Internal EGT sensor
  • Ignition from the internal spark plug
  • Optical rotation measurement

Dimensions: length 315mm diameter 115mm

Weight of the whole set (engine + equipment): 1750g

 

  • Amplifier board with RPM and EGT sensors. Mounted on the engine.
  • Engine management and control module ProJET model HORNET III or newer. (ECU)
  • LCD panel for operating and programming turbine parameters. (GSU)
  • Fuel gear pump with 4mm pipe terminals.
  • Main and starting fuel valves.
  • A set of 4mm hydraulic pipes.
  • A set of electrical wires
  • MPX plug with adapter plate for battery connection.

 

Engine GTM 160

160N static thrust engine with or without equipment. Automatic start with liquid fuel (internal "kerostart"). Thermal protection of the turbine bearing by using an aluminum-steel shaft sleeve. The latest bearing lubrication system with directional air flow. A mounting bracket is supplied with the engine. The version with equipment has a microprocessor-based control module, interface for programming and parameter reading, fuel pump, starting and main fuel solenoid valves, electric and fuel lines. The product is intended for modeling applications. Requires careful reading of the safe use instructions. It may be a serious threat to health and life if used improperly.

with equipment:

9400zł

|

without equipment:

7900zł

Parameters

Static thrust: 160N (w praktyce do 170N)

Rotor speed at max power: 120 000rpm

Minimum rotor speed: 33,000 rpm

Fuel consumption: 400 g/min (at maximum thrust)

  • Supply: JET A1 + 3-5% MOBIL Jet Oil II, AEROSHELL 500/560
  • Automatic start "kerostart"
  • Built-in starter
  • Internal EGT sensor
  • Ignition from the internal spark plug
  • Optical rotation measurement

Dimensions: length 315mm diameter 115mm

Weight of the whole set (engine + equipment): 1770g

 

  • Amplifier board with RPM and EGT sensors. Mounted on the engine.
  • Engine management and control module ProJET model HORNET III or newer. (ECU)
  • LCD panel for operating and programming turbine parameters. (GSU)
  • Fuel gear pump with 4mm pipe terminals.
  • Main and starting fuel valves.
  • A set of 4mm hydraulic pipes.
  • A set of electrical wires
  • MPX plug with adapter plate for battery connection.

 

Engine GTM 180

180N static thrust engine with or without equipment. Automatic start with liquid fuel (internal "kerostart"). Thermal protection of the turbine bearing by using an aluminum-steel shaft sleeve. The latest bearing lubrication system with directional air flow. A mounting bracket is supplied with the engine. The version with equipment has a microprocessor-based control module, interface for programming and parameter reading, fuel pump, starting and main fuel solenoid valves, electric and fuel lines. The product is intended for modeling applications. Requires careful reading of the safe use instructions. It may be a serious threat to health and life if used improperly.

with equipment:

9900zł

|

without equipment:

8600zł

Parameters

Static thrust: 180N

Rotor speed at max power: 120 000rpm

Minimum rotor speed: 33,000 rpm

Fuel consumption: 430 g/min

  • Supply: JET A1 + 3-5% MOBIL Jet Oil II, AEROSHELL 500/560
  • Automatic start "kerostart"
  • Built-in starter
  • Internal EGT sensor
  • Ignition from the internal spark plug
  • Optical rotation measurement

Dimensions: length 315mm diameter 115mm

Weight of the whole set (engine + equipment): 1790g

 

  • Amplifier board with RPM and EGT sensors. Mounted on the engine.
  • Engine management and control module ProJET model HORNET III or newer. (ECU)
  • LCD panel for operating and programming turbine parameters. (GSU)
  • Fuel gear pump with 4mm pipe terminals.
  • Main and starting fuel valves.
  • A set of 4mm hydraulic pipes.
  • A set of electrical wires
  • MPX plug with adapter plate for battery connection.

 

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Design and realization: Aggie Studio