TH-WP100 Turbojet Engine

TH-WP100 Turbojet Engine
Details:
High Thrust TH-WP100 Turbojet Engine Overview The TH-WP100 turbojet engine delivers a maximum static thrust of 95 kgf under ISA conditions. It is a mature, high-power single-shaft turbojet designed for high-speed unmanned aerial platforms. Balancing reliable thrust output, compact dimension and...
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Xpert Intelligent Equipment Co., Ltd. is one of the leading manufacturers and suppliers of th-wp100 turbojet engine in China. We have world-leading production equipment and strong manufacturing capabilities. Welcome to wholesale bulk cheap th-wp100 turbojet engine in stock here from our factory. Customized orders are welcome.

 

High Thrust TH-WP100 Turbojet Engine Overview

 

TH-WP UAV turbojet engine with controller cable white background product image

The TH-WP100 turbojet engine delivers a maximum static thrust of 95 kgf under ISA conditions. It is a mature, high-power single-shaft turbojet designed for high-speed unmanned aerial platforms. Balancing reliable thrust output, compact dimension and strong overload resistance, this turbojet is widely adopted for target drones, high-speed UAVs and aerospace research projects. With a max flight altitude up to 12000 m and 6 g maneuver overload capability, it performs stably in high-speed cruise and agile flight missions.

 

 

 

Core Advantages of TH-WP100 Turbojet Motor

 

95kgf Stable Thrust Output:

Consistent power under standard atmospheric conditions, ideal for large high-speed UAV platforms.

High Overload Resistance:

Supports 6g maneuver overload and 25g impact overload, adapts to harsh flight conditions.

Wide Envelope Flight Performance:

Max working altitude reaches 12000m, suitable for high-altitude high-speed missions.

Compact Integrated Structure:

Diameter 202mm, length 508mm, easy for airframe integration and installation.

Clear Maintenance Schedule:

25-hour maintenance cycle, convenient for routine inspection and after-service management.

Controllable Fuel Consumption:

Clear SFC & fuel flow data for overall aircraft power system simulation.

 

 

 

TH-WP100 Turbojet Engine Technical Specifications

 

Item Parameter Unit
Thrust@max rpm (ISA Conditions) 95 kgf
SFC@max rpm 1.45 kg/kgf·h
Fuel Consumption@max rpm 2.95 L/min
Weight 11.5 kg
Diameter 202 mm
Length 508 mm
Idle Speed 24000 rpm
Max Speed 64000 rpm
Mass Flow 1.6 kg/s
Pressure Ratio 4.0 -
Max Exhaust Gas Temperature 780 ℃
Max Flight Altitude 12000 m
Max Maneuvering Overload 6 g
Max Impact Overload 25 g
Maintenance Period 25 h
TH-WP UAV turbojet engine with controller cable white background product image

 

 

 

TH-WP100 Turbojet Engine Application Scenarios
 
High-Speed Target Drones

High-Speed Target Drones

Perfect for aerial target simulation for air defense test and training. Stable high-speed performance meets repeated interception test requirements.

Large High-Speed Unmanned Aerial Vehicles

Serves as the core power plant for high-speed reconnaissance UAV, strike UAV platforms with heavy payload demand.

Aerial Reconnaissance Rapid Response Missions
Aerospace Scientific Research Testing

Aerospace Scientific Research & Test Projects

Used in university and research institute aerodynamic tests, flight verification projects, power system simulation experiments.

Custom High-Speed Aircraft Prototype

Supports custom airframe matching for experimental jet platforms, provides stable and verifiable thrust data for design iteration.

Custom Jet-Powered Aerial Platforms

 

 

 

 

Customization & Bulk Order Service for TH-WP100 Turbojet

We support bulk supply of TH-WP100 turbojet engines for global B2B buyers.

Custom modification: Interface adjustment, sensor configuration, test report support upon request.

Batch delivery: Stable factory supply, customizable packaging and export documents.

Technical support: Dedicated engineering team for integration guidance, startup & flight debugging assistance.

After-sales: Standard maintenance guidance, spare parts supply for long-term cooperation clients.

 

 

 

 

FAQ

Q: What fuel does the TH-WP100 turbojet use?

A: It works with standard aviation kerosene, please follow our operation manual for fuel selection.

Q: What is the maximum operating altitude of this 95kgf turbojet?

A: The max flight altitude is 12000 meters. Thrust will drop naturally with altitude rising.

Q: Can you provide test data and inspection certificate for each unit?

A: Yes, we can provide factory test report for each engine for engineering review.

Q: Is technical guidance available after delivery?

A: We provide remote technical support for engine installation, startup and routine maintenance.

Q: What is the service life definition of the 25-hour maintenance cycle?

A: The 25-hour maintenance period refers to the scheduled inspection interval. It is not the total service life of the engine. After professional inspection and overhaul, the engine can continue to operate.

Q: Does this engine come with an ECU and supporting control system?

A: Standard version is matched with dedicated engine controller. We can supply the complete control set or deliver the bare engine separately according to your order requirements.

 

 

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