GE F35E00HAHF8FH6DM8HP6DUXXW6C F135-PW-600 Engine Variant
GE F35E00HAHF8FH6DM8HP6DUXXW6C F135-PW-600 Engine Variant
Manufacturer: General Electric
Product No.: F35E00HAHF8FH6DM8HP6DUXXW6C
Condition:1000 in stock
Product Type: F135-PW-600 Engine Variant
Product Origin: USA
Payment: T/T, Western Union
Weight: 1000g
Shipping port: Xiamen
Warranty: 12 months
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Product Details
| Parameter | Details |
|---|---|
| Manufacturer | General Electric |
| Model/Part Number | F35E00HAHF8FH6DM8HP6DUXXW6C |
| Description | F135-PW-600 Engine Variant |
Product Overview
| Parameter | Details |
|---|---|
| Part Number | F35E00HAHF8FH6DM8HP6DUXXW6C |
| Product Name | F135 Engine (F-35 Lightning II Variant) |
| Application | Powerplant for the F-35 Lightning II Joint Strike Fighter, providing propulsion for stealth fighter aircraft |
| Compatibility | Designed for Lockheed Martin F-35 variants (F-35A, F-35B, F-35C); supports STOVL (Short Take-Off and Vertical Landing) operations |
| Function | High-bypass turbofan engine with afterburner, delivering thrust for supersonic flight, vertical lift, and integrated power for aircraft systems |
Functional Specifications
| Parameter | Details |
|---|---|
| Engine Type | Afterburning turbofan with adaptive cycle technology |
| Thrust (Dry) | 28,000 lbf (125 kN) |
| Thrust (Afterburner) | 43,000 lbf (191 kN) |
| Bypass Ratio | 0.57:1 |
| Length | 17.3 ft (5.28 m) |
| Diameter | 46 in (1.17 m) |
| Dry Weight | 3,750 lb (1,701 kg) |
| Overall Pressure Ratio | 28:1 |
| Turbine Inlet Temperature | 3,600°F (1,980°C) |
| Fuel Type | JP-8 or equivalent |
| Maintenance Interval | 2,000 flight hours |
| Standards Compliance | MIL-STD-881, FAA certification, NATO STANAG |
Product Description
Product Details
| Parameter | Details |
|---|---|
| Manufacturer | General Electric |
| Model/Part Number | F35E00HAHF8FH6DM8HP6DUXXW6C |
| Description | F135-PW-600 Engine Variant |
Product Overview
| Parameter | Details |
|---|---|
| Part Number | F35E00HAHF8FH6DM8HP6DUXXW6C |
| Product Name | F135 Engine (F-35 Lightning II Variant) |
| Application | Powerplant for the F-35 Lightning II Joint Strike Fighter, providing propulsion for stealth fighter aircraft |
| Compatibility | Designed for Lockheed Martin F-35 variants (F-35A, F-35B, F-35C); supports STOVL (Short Take-Off and Vertical Landing) operations |
| Function | High-bypass turbofan engine with afterburner, delivering thrust for supersonic flight, vertical lift, and integrated power for aircraft systems |
Functional Specifications
| Parameter | Details |
|---|---|
| Engine Type | Afterburning turbofan with adaptive cycle technology |
| Thrust (Dry) | 28,000 lbf (125 kN) |
| Thrust (Afterburner) | 43,000 lbf (191 kN) |
| Bypass Ratio | 0.57:1 |
| Length | 17.3 ft (5.28 m) |
| Diameter | 46 in (1.17 m) |
| Dry Weight | 3,750 lb (1,701 kg) |
| Overall Pressure Ratio | 28:1 |
| Turbine Inlet Temperature | 3,600°F (1,980°C) |
| Fuel Type | JP-8 or equivalent |
| Maintenance Interval | 2,000 flight hours |
| Standards Compliance | MIL-STD-881, FAA certification, NATO STANAG |