SPECIFICATIONS:

• Type: Axial flow two-spool turbojet
• Length: 152.2 in (387 cm)
• Diameter: 40 in (100 cm)
• Dry weight: 3,615 lb (1,640 kg)

COMPONENTS:
 

• Compressor:Axial 6 LP pressure stages, 8 HP stages
• Combustors:Cannular 10 flame tubes
• Turbine:HP single stage, LP single stage
• Fuel type:AVTUR or AVTAG

PERFORMANCE:

• Maximum thrust:11,000 lbf (49 kN)
• Specific fuel consumption:.817 lb/(lbf·h) (23.1 g/(kN·s))
• Power-to-weight ratio:3.04:1

FEATURES:
 

• Real perfect engine
• With accessories are fixed
• Movable stand
• Easy top visible all the accessories

• 13 cylinders- Rotary   type
• Rotary  type  cylinder arrangement
• Cut section/without Cut Section
• With /Without Electrical power test
•  Motor-1HP
• With Stand setup 

• Aircraft engine running module
• Less weight
• Easy Movable
• Easily Assemble and dismantle 

SPECIFICATIONS:

• 4 cylinders- Horizontally Opposed type
• Horizontally Opposed type cylinder arrangement
• Cut section/without Cut Section
• With /Without Electrical power test
•  Motor-1HP
• With Stand setup

FEATURES:

• Aircraft engine running module
• Less weight
• Easy Movable
• Easily Assemble and dismantle
• Easily visible Piston movements

SPECIFICATIONS:

• Type: turbojet
• Length: 4.039 m (13 ft 3 in)
• Diameter: 1.212 m (47.75 in)
• Dry weight: 3,175 kg (7,000 lb)

COMPONENTS:

• Compressor: Axial flow, 7-stage low pressure, 7-stage high pressure
• Combustors: Nickel alloy construction annular chamber, 16 vapourising burners, each with twin outlets
• Turbine: High pressure single stage, low pressure single stage
• Fuel type: Jet A1

FEATURES:

• Real perfect engine
• With accessories are fixed
• Movable stand
• Easy top visible all the accessories

TECHNICAL SPECIFICATION

• Type: Turbofan
• Length: 3,600 millimeters (142 in)
• Diameter: 720 millimeters (28.3 in)
• Dry weight: 976 kilograms (2,151 lb)

• Compressor: 3-stage LP, 3-stage IP, 6-stage HP
• Turbine: Single stage HP, Single stage IP, 2-stage LP

• Maximum thrust: 40 kilonewtons (9,100 lbf) dry,73 kilonewtons (16,400 lbf)
• Overall pressure ratio: 23.5:1
• Bypass ratio: 1.1:1
• Thrust-to-weight ratio: 7.6:1 (with reheat)

FEATURES:

• Real perfect engine
• With accessories are fixed
• Movable stand
• Easy top visible all the accessories

SPECIFICATIONS:

• 9 cylinders- Radial type
• Radial Type cylinder arrangement
• Cut section/without Cut Section
• With /Without Electrical power test
• Motor-1HP
• With Stand setup
• Piston heads with rings

• Aircraft engine running module
• Less weight
• Easy Movable
• Easily Assemble and dismantle

SPECIFICATIONS:

• 4 cylinders- Horizontally Opposed type
• Horizontally Opposed type cylinder arrangement
• Cut section/without Cut Section
• With /Without Electrical power test
• Motor-1HP
• With Stand setup

FEATURES:

• Aircraft engine running module
• Less weight
• Easy Movable
• Easily Assemble and dismantle