Titan E-start with 40 Kg (392N / 88Lbf) thrust. PRE ORDER ONLY, PRODUCTION NEEDS AROUND 20-30DAYS. EMAIL TO US TO CONFIRM

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust. PRE ORDER ONLY, PRODUCTION NEEDS AROUND 20-30DAYS. EMAIL TO US TO CONFIRM

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust. PRE ORDER ONLY, PRODUCTION NEEDS AROUND 20-30DAYS. EMAIL TO US TO CONFIRM

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Titan E-start with 40 Kg (392N / 88Lbf) thrust.

To celibrate AMT Netherlands 12,5 th Anniversary of series production we introduced a new engine in the high thrust class.

Description of the Titan Electric start gas turbine.

The Titan has been constructed from a single radial compressor and an axial flow turbine stage. The Titan owes much of its excellent performance and superb power/weight ratio to a new design diffuser stage. This revolutionary type of diffuser also allows the relative small engine diameter.

The time required for the Titan to spool up and down is also positively influenced by the low mass of the axial turbine wheel, taking less than 4 seconds and from min. to max. rpm and only 3 seconds from max. rpm to min. rpm.

Like all our turbines the Titan is available with manual or auto Air-start, as well as fully automatic electric starting.

Pre Order Only.

EPV layout.

EPV stands for Ecu-Pump-Valves all together in one aluminium casing. The EPV is connected with a 50 cm long cable, using a high quality Amphenol connector, to the side of the Nike engine. The control of the engine with this EPV can be done in 3 different ways. 1 With a PWM signal 2. With a DC signal (analog control) 3. With a serial protocol. More information about the EPV layout will follow shortly.

Description.

The Nike engine is a direct "spin-off" of the successful Titan engine, knowledge collected during the last 5 years of building and testing the Titan engine did evaluate into another revolutionary design gas turbine.

Construction.

The Nike engine is constructed around a single, fully CNC machined, radial compressor wheel and an axial flow turbine stage. The Nike owes most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to the Titan engine.

Fuel consumption.

The specific fuel consumption is extremely good for an engine in this thrust class especially when looking at the small engine diameter of this engine. At S.T.P. and 100% throttle (784N/176Lbf thrust) this engine uses only 1850 Gram/Min (65,25 oz/min). You will not find an engine with better fuel consumption figures.

Seize / weight.

The diffuser stage allows the relative small engine diameter of 201 mm for this high thrust engine. The "engine only weight" is 9150 gram (20,2 Lb), the "system airborne * weight" of the complete Nike system is only 11300 gram (24,9 Lb), which is extremely competitive for an engine with this thrust.

Starting system.

Since March 2014 the Nike is already manufactured with a internal direct electric start kerosene starting system, on request also propane start is a option, both work as a fully automatic electric starting system.

Features.

A feature used within this engine is the internal EGT sensor, this EGT sensor (a real Tt5) has a diameter of 1.0 mm, because of this small diameter there is a fast EGT response time possible. The result of this fast EGT response time is a short start up time of less than 30 seconds.

Applications.

This engine will find its use in UAV high speed target drone applications, experimental aircraft, universities, sound studies, full size gliders and many more applications. Especially for "university" applications we can apply several measuring positions on this engine like we do with Olympus HP and Titan engines. (see picture of a University Olympus HP engine)

Pricing.

The price mentioned in our pricing page is a single unit priceing. For our dealer network and larger quantities we can offer a different pricing.

Restrictions.

There are no restrictions for the sale of this engine within the European Union **), however for customers outside the European Union there is a need for a "end user certificate". This certificate is needed because of Counsel Regulation (EC) No 1167/2008 of 24 October 2008, more specific; CATEGORY 9 AEROSPACE AND PROPULSION.

Production.

AMT Netherlands did start with the production the engine layout with EPV middle October 2014.

*) Total weight of; Nike engine, EPV, 5200 Mah LiPo battery, mounting straps.
**) For countries see European Union site

ECU, fuel pump, solenoid valves.

The original Nike configuration with separate ECU, fuel pump and solenoid valves is still available. Previous systems can be converted to the EPV layout, contact AMT Netherlands for a quotation.

EPV layout.

EPV stands for Ecu-Pump-Valves all together in one aluminium casing. The EPV is connected with a 50 cm long cable, using a high quality Amphenol connector, to the side of the Nike engine. The control of the engine with this EPV can be done in 3 different ways. 1 With a PWM signal 2. With a DC signal (analog control) 3. With a serial protocol. More information about the EPV layout will follow shortly.

Description.

The Nike engine is a direct "spin-off" of the successful Titan engine, knowledge collected during the last 5 years of building and testing the Titan engine did evaluate into another revolutionary design gas turbine.

Construction.

The Nike engine is constructed around a single, fully CNC machined, radial compressor wheel and an axial flow turbine stage. The Nike owes most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to the Titan engine.

Fuel consumption.

The specific fuel consumption is extremely good for an engine in this thrust class especially when looking at the small engine diameter of this engine. At S.T.P. and 100% throttle (784N/176Lbf thrust) this engine uses only 1850 Gram/Min (65,25 oz/min). You will not find an engine with better fuel consumption figures.

Seize / weight.

The diffuser stage allows the relative small engine diameter of 201 mm for this high thrust engine. The "engine only weight" is 9150 gram (20,2 Lb), the "system airborne * weight" of the complete Nike system is only 11300 gram (24,9 Lb), which is extremely competitive for an engine with this thrust.

Starting system.

Since March 2014 the Nike is already manufactured with a internal direct electric start kerosene starting system, on request also propane start is a option, both work as a fully automatic electric starting system.

Features.

A feature used within this engine is the internal EGT sensor, this EGT sensor (a real Tt5) has a diameter of 1.0 mm, because of this small diameter there is a fast EGT response time possible. The result of this fast EGT response time is a short start up time of less than 30 seconds.

Applications.

This engine will find its use in UAV high speed target drone applications, experimental aircraft, universities, sound studies, full size gliders and many more applications. Especially for "university" applications we can apply several measuring positions on this engine like we do with Olympus HP and Titan engines. (see picture of a University Olympus HP engine)

Pricing.

The price mentioned in our pricing page is a single unit priceing. For our dealer network and larger quantities we can offer a different pricing.

Restrictions.

There are no restrictions for the sale of this engine within the European Union **), however for customers outside the European Union there is a need for a "end user certificate". This certificate is needed because of Counsel Regulation (EC) No 1167/2008 of 24 October 2008, more specific; CATEGORY 9 AEROSPACE AND PROPULSION.

Production.

AMT Netherlands did start with the production the engine layout with EPV middle October 2014.

*) Total weight of; Nike engine, EPV, 5200 Mah LiPo battery, mounting straps.
**) For countries see European Union site

ECU, fuel pump, solenoid valves.

The original Nike configuration with separate ECU, fuel pump and solenoid valves is still available. Previous systems can be converted to the EPV layout, contact AMT Netherlands for a quotation.

PRE ORDER ONLY FOR INDUSTRIAL CUSTOMER PRODUCTION TIME AROUND 25-40 DAYS

EPV layout.

EPV stands for Ecu-Pump-Valves all together in one aluminium casing. The EPV is connected with a 70 cm long cable, using a high quality military spec.connector, to the side of the lynx engine. The control of the engine with this EPV can be done in 3 different ways. 1 With a PWM signal 2. With a DC signal (analog control) 3. With a serial protocol. More information about the EPV layout will follow shortly.

Description.

The lynx engine is a direct "spin-off" of the successful Nike engine, knowledge collected during the last 4 years of building and testing the Lynx engine did evaluate into another revolutionary design gas turbine.

Construction.

The Lynx engine is constructed around a single, fully in house CNC machined, radial compressor wheel and an axial flow turbine stage. The Lynx engine owns most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to the Nike engine.

Fuel consumption.

The specific fuel consumption is extremely good for an engine in this thrust class especially when looking at the small engine diameter of this engine. At S.T.P. and 100% throttle (1569N/352Lbf thrust) the Lynx engine uses only 3600 Gram/Min (127 oz/min) of fuel.

Seize / weight.

The diffuser stage allows the relative small engine diameter of 261,4 mm for this high thrust engine. The "engine only weight" is 19500 gram (43 Lb), the "system airborne *) weight" of the complete Lynx system is 24280 gram (53,5 Lb), which is extremely competitive for an engine with this thrust, you will not find an engine in this thrust class with better power to weight ratio.

Starting system.

The Lynx engine is manufactured with an dual internal igniter system which allows a relaiable fully automatic start.

Features.

A other feature used within the Lynx engine are the 2 internal EGT sensors, these 2 induvidual monitored EGT sensors (both a real Tt5) have both a small diameter of 1.5 mm, because of this small diameter there is a fast EGT response time possible. The result of this fast EGT response time is a short start up time of less than 45 seconds.

Applications.

This engine will find its use in large UAV high speed target drone applications, experimental aircraft, universities, sound studies, full size gliders and many more applications. Especially for "university" applications we can apply several measuring positions on this engine like we do with Olympus HP and Titan engines. (see picture of a University Olympus HP engine)

Pricing.

The price mentioned in our pricing page is a single unit priceing. For our dealer network and larger quantities we can offer a different pricing.

Restrictions.

There are no restrictions for the sale of this engine within the European Union **), however for customers outside the European Union there is a need for a "end user certificate". This certificate is needed because of Counsel Regulation (EC) No 1167/2008 of 24 October 2008, more specific; CATEGORY 9 AEROSPACE AND PROPULSION.

Production.

AMT Netherlands did start the actual production process of this engine in the Version 3 EPV layout, end of the year 2018.

Complete package.

The Lynx engine will be shipped as a "ready to run" complete package

Future developments.

For the future AMT Netherlands will develop a brushless starter/generator combination (500-1000 Watt of power) and has plans to develop an internal, oil based, lubrication system for this engine to increase MTBO.

*) Total weight of; Lynx engine, Connecting cable, Version 3 EPV, 4500 Mah 6S LiPo battery, AMT-NL Lynx fuel filter, 3 x mounting strap.
**) For countries see European Union site

Complete packageThe AMT Netherlands Lynx turbine will be shipped in a flight case to protect for shipping damage, all is ready to install and run. Each shipment includes: 2 intergrated Thermocouples. Version 3 EPV Unit. 6 cell Lipo battery for EPV. Engine log and warranty card (2 Years). 3 Mounted Stainless-steel mounting brackets. 2 intergrated igniters. Telemetry software. Engine Data Terminal (EDT). Amphenol military spec.connectors. A fully operational Lynx gas turbine. Engine test data. Lynx high flow fuel filter. Telemetry software. 3 types of tubing. Battery charging cable. Front and rear engine protection covers. Owners Manual.

EPV layout.

EPV stands for Ecu-Pump-Valves all together in one aluminium casing. The EPV is connected with a 70 cm long cable, using a high quality military spec.connector, to the side of the lynx engine. The control of the engine with this EPV can be done in 3 different ways. 1 With a PWM signal 2. With a DC signal (analog control) 3. With a serial protocol. More information about the EPV layout will follow shortly.

Description.

The lynx engine is a direct "spin-off" of the successful Nike engine, knowledge collected during the last 4 years of building and testing the Lynx engine did evaluate into another revolutionary design gas turbine.

Construction.

The Lynx engine is constructed around a single, fully in house CNC machined, radial compressor wheel and an axial flow turbine stage. The Lynx engine owns most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to the Nike engine.

Fuel consumption.

The specific fuel consumption is extremely good for an engine in this thrust class especially when looking at the small engine diameter of this engine. At S.T.P. and 100% throttle (1569N/352Lbf thrust) the Lynx engine uses only 3600 Gram/Min (127 oz/min) of fuel.

Seize / weight.

The diffuser stage allows the relative small engine diameter of 261,4 mm for this high thrust engine. The "engine only weight" is 19500 gram (43 Lb), the "system airborne *) weight" of the complete Lynx system is 24280 gram (53,5 Lb), which is extremely competitive for an engine with this thrust, you will not find an engine in this thrust class with better power to weight ratio.

Starting system.

The Lynx engine is manufactured with an dual internal igniter system which allows a relaiable fully automatic start.

Features.

A other feature used within the Lynx engine are the 2 internal EGT sensors, these 2 induvidual monitored EGT sensors (both a real Tt5) have both a small diameter of 1.5 mm, because of this small diameter there is a fast EGT response time possible. The result of this fast EGT response time is a short start up time of less than 45 seconds.

Applications.

This engine will find its use in large UAV high speed target drone applications, experimental aircraft, universities, sound studies, full size gliders and many more applications. Especially for "university" applications we can apply several measuring positions on this engine like we do with Olympus HP and Titan engines. (see picture of a University Olympus HP engine)

Pricing.

The price mentioned in our pricing page is a single unit priceing. For our dealer network and larger quantities we can offer a different pricing.

Restrictions.

There are no restrictions for the sale of this engine within the European Union **), however for customers outside the European Union there is a need for a "end user certificate". This certificate is needed because of Counsel Regulation (EC) No 1167/2008 of 24 October 2008, more specific; CATEGORY 9 AEROSPACE AND PROPULSION.

Production.

AMT Netherlands did start the actual production process of this engine in the Version 3 EPV layout, end of the year 2018.

Complete package.

The Lynx engine will be shipped as a "ready to run" complete package

Future developments.

For the future AMT Netherlands will develop a brushless starter/generator combination (500-1000 Watt of power) and has plans to develop an internal, oil based, lubrication system for this engine to increase MTBO.

*) Total weight of; Lynx engine, Connecting cable, Version 3 EPV, 4500 Mah 6S LiPo battery, AMT-NL Lynx fuel filter, 3 x mounting strap.
**) For countries see European Union site

Complete packageThe AMT Netherlands Lynx turbine will be shipped in a flight case to protect for shipping damage, all is ready to install and run. Each shipment includes: 2 intergrated Thermocouples. Version 3 EPV Unit. 6 cell Lipo battery for EPV. Engine log and warranty card (2 Years). 3 Mounted Stainless-steel mounting brackets. 2 intergrated igniters. Telemetry software. Engine Data Terminal (EDT). Amphenol military spec.connectors. A fully operational Lynx gas turbine. Engine test data. Lynx high flow fuel filter. Telemetry software. 3 types of tubing. Battery charging cable. Front and rear engine protection covers. Owners Manual.