Product Description
Product Details
| Parameter | Details |
|---|---|
| Manufacturer | General Electric |
| Model/Part Number | F35E00HCHF8LH67M8NP6DUXXWXX |
| Description | F135 Engine Variant |
Product Overview
| Parameter | Details |
|---|---|
| Part Number | F35E00HCHF8LH67M8NP6DUXXWXX |
| Product Name | F135-PW-600 Core Engine Module |
| Application | Propulsion system for the F-35 Lightning II Joint Strike Fighter, enabling high-performance flight in stealth fighter aircraft |
| Compatibility | Lockheed Martin F-35 variants (F-35A, F-35B, F-35C); supports STOVL operations with lift fan integration |
| Function | High-bypass afterburning turbofan engine delivering thrust for supersonic cruise, vertical takeoff/landing, and integrated aircraft power generation |
Functional Specifications
| Parameter | Details |
|---|---|
| Engine Type | Adaptive cycle afterburning turbofan with three-stream architecture |
| Thrust (Dry) | 28,000 lbf (125 kN) |
| Thrust (Afterburner) | 43,000 lbf (191 kN) |
| Bypass Ratio | Variable 0.57:1 to 1.0:1 (adaptive) |
| 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 jet fuel |
| Maintenance Interval | 2,000 flight hours (with advanced health monitoring) |
| Standards Compliance | MIL-STD-881, FAA Type Certification, NATO STANAG compliant |