Turkish Engine Programs

[Oguzbalasi]

it's not a turboprop, it's diesel engine. Gezgin as other cruise missiles needs turboJET.

 

[xbat]

are you sure? that is not pd170(or pd220). it is so called turboprop engine for AKINCI . i cant verify it but nobody deny it until today, so i can say photo is real.

 

[Successwill]

are you sure? that is not pd170(or pd220). it is so called turboprop engine for AKINCI . i cant verify it but nobody deny it until today, so i can say photo is real.

We dont need anyone to deny it. We can say it is a diesel engine by its look..

 

[xbat]

http://www.kokpit.aero/akinci-iha-tei-motoru

 

[Oguzbalasi]

it's a diesel engine, period.

 

[-------]

Kale 3200 Turbojet

Engine Specifications:
Type:Single Spool Turbojet
Major Applications: SOM ALCM Family and ATMACA Block I/II Missiles
Fully Functional Prototypes Delivery: Two prototypes in 2019
Length:~ 70 cm
Diameter: 30 cm
Dry Weight:48 kg
Specific Fuel Consumption (SFC): < or = 1.2 kg/daN/hr
Compressor: Various configurations have been studied during design phase including 4-stage axial, 5-stage axial and 1 axial and 1 radial compressor combination
Turbine: Single Stage
Fuel Type: JP8, JP10
Lubrication System: The bearing system is lubricated by fuel (on board the missile) rather than a separate oil system
Generator: Permanent magnet based 6kVA generator mounted on the engine shaft
Maximum Thrust: 3.2 kN (787 lbf)
Speed: Kale 3200 is designed to provide Mach 0.95 flight speed on SOM ALCM at a 5,000 ft altitude
Service Life: 17 hours
Running Time on SOM Missile: 20 to 25 minutes
First Test on a Test Bench at Laboratory: September 19, 2013

 

[Oublious]

Kale 3200 Turbojet
View attachment 518819
Engine Specifications:
Type:Single Spool Turbojet
Major Applications: SOM ALCM Family and ATMACA Block I/II Missiles
Fully Functional Prototypes Delivery: Two prototypes in 2019
Length:~ 70 cm
Diameter: 30 cm
Dry Weight:48 kg
Specific Fuel Consumption (SFC): < or = 1.2 kg/daN/hr
Compressor: Various configurations have been studied during design phase including 4-stage axial, 5-stage axial and 1 axial and 1 radial compressor combination
Turbine: Single Stage
Fuel Type: JP8, JP10
Lubrication System: The bearing system is lubricated by fuel (on board the missile) rather than a separate oil system
Generator: Permanent magnet based 6kVA generator mounted on the engine shaft
Maximum Thrust: 3.2 kN (787 lbf)
Speed: Kale 3200 is designed to provide Mach 0.95 flight speed on SOM ALCM at a 5,000 ft altitude
Service Life: 17 hours
Running Time on SOM Missile: 20 to 25 minutes
First Test on a Test Bench at Laboratory: September 19, 2013

sexy...

 

[rajvoSa]

So much great news in such short period of time.

 

[SİLAHDAR]

Kale 3200 Turbojet
View attachment 518819
Engine Specifications:
Type:Single Spool Turbojet
Major Applications: SOM ALCM Family and ATMACA Block I/II Missiles
Fully Functional Prototypes Delivery: Two prototypes in 2019
Length:~ 70 cm
Diameter: 30 cm
Dry Weight:48 kg
Specific Fuel Consumption (SFC): < or = 1.2 kg/daN/hr
Compressor: Various configurations have been studied during design phase including 4-stage axial, 5-stage axial and 1 axial and 1 radial compressor combination
Turbine: Single Stage
Fuel Type: JP8, JP10
Lubrication System: The bearing system is lubricated by fuel (on board the missile) rather than a separate oil system
Generator: Permanent magnet based 6kVA generator mounted on the engine shaft
Maximum Thrust: 3.2 kN (787 lbf)
Speed: Kale 3200 is designed to provide Mach 0.95 flight speed on SOM ALCM at a 5,000 ft altitude
Service Life: 17 hours
Running Time on SOM Missile: 20 to 25 minutes
First Test on a Test Bench at Laboratory: September 19, 2013

How many years take for make a tr-60-30 like engine with this experiment and base technology ?

 

[mehmet75]

0,95 mach at 5000 ft altitude for 25 minutes, makes about : 450 km.

I guess in some conditions (altitude, no sharp manoeuvres, tail wind etc.) , SOM may go 500 km..

 

[Test7]

 

[Mert_Ank]

1.57... ya... motoru , ya ... moturu , o da geliyor insallah , ne diyor orda?

 

[Mert_Ank]

More technical info

 

[-------]

So Rolls Royce is out?

It seems that way yes..

A joint venture company TAEC, 51% Kale Group and 49% Rolls-Royce..

 

[rajvoSa]

Im a bit sceptical on the subjects. I kinda got a vibe that RR is not out, but their role will be less public, as a silent partner. I dont believe in coincidences, visits of UK defence ministers was surely at least in part had to do with the project. Also RR isnt only company linked and willing to take part in the project, BAE is commited to, and dont forget that Nurol -BAE just recently started a nwe company specifially for devolment and producrion of sub systems for this project.

Last bot not least, UK companies were exluded from future German -France fighter project, cosequenxes of BREXIT. On which UK responded that they are already involved in TF-X.