Xpert Intelligent Equipment Co., Ltd. is one of the leading manufacturers and suppliers of th-wp160 turbojet engine in China. We have world-leading production equipment and strong manufacturing capabilities. Welcome to wholesale bulk cheap th-wp160 turbojet engine in stock here from our factory. Customized orders are welcome.
High-Thrust Turbojet Engine TH-WP160 Overview
The TH-WP160 turbojet engine delivers a rated maximum thrust of 162 kgf under ISA conditions, built for high-speed, high-altitude unmanned aerial platforms that demand stable, sustained power output. Different from medium-thrust turbojet models for small test drones, this 160-class unit is engineered for heavy airframes with strict overload and high-altitude performance requirements.
It features a compact single-stage turbojet layout with optimized aerodynamic design, supporting continuous operation up to 12,000 m altitude and enduring up to 6g maneuver overload. Tuned for low specific fuel consumption at max RPM, it balances thrust efficiency and flight duration for long-range cruise missions. The robust mechanical structure is certified for 25g impact overload, making it reliable for harsh launch and recovery scenarios.
Core Advantages of 162kgf Turbojet for High-Speed UAV
High Thrust-to-Weight Performance
162 kgf peak thrust with 22.5 kg engine weight, ideal for heavy high-speed platforms that require rapid acceleration.
Excellent High-Altitude Adaptability
Stable power retention at 12,000 m, suitable for subsonic & supersonic target drone and long-endurance cruise missions.
High Overload Resistance
6g continuous maneuver overload + 25g impact overload, survives catapult launch, air drop and high-G flight profiles.
Optimized Fuel Economy
SFC down to 1.35 kg/kgf·h at max speed, reduces fuel load pressure and extends effective flight range.
Mature Thermal Management
Max exhaust temperature controlled at 780℃, stable long-time continuous operation with 25-hour maintenance interval.
Compact Integrated Structure
261mm diameter, 646mm length, convenient for airframe integration and modular installation.
TH-WP160 Turbojet Engine Technical Specifications
| Item | Specification | Unit |
|---|---|---|
| Thrust@max rpm (ISA Conditions) | 162 | kgf |
| SFC@max rpm | 1.35 | kg/kgf·h |
| Fuel Consumption@max rpm | 4.56 | L/min |
| Weight | 22.5 | kg |
| Diameter | 261 | mm |
| Length | 646 | mm |
| Idle Speed | 20000 | rpm |
| Max Speed | 55000 | rpm |
| Mass Flow | 2.7 | kg/s |
| Pressure Ratio | 4.5 | - |
| Max Exhaust Gas Temperature | 780 | ℃ |
| Max Flight Altitude | 12000 | m |
| Max Maneuvering Overload | 6 | g |
| Max Impact Overload | 25 | g |
| Maintenance Period | 25 | h |
Application Scenarios for 162kgf Turbojet Engine
High-Speed Supersonic / Subsonic Target Drones
The primary application: full-size aerial target systems for air defense weapon testing, simulating fighter jet flight signatures, high-G maneuvers and high-altitude penetration profiles.
Long-Range High-Speed Cruise UAV
For heavy payload reconnaissance, simulation and cruise platforms requiring sustained high-speed flight above 8000 m.
Aerospace Research & Flight Test Platforms
University and research institute test beds for aerodynamic, fuel system and flight control validation under high-altitude, high-speed conditions.
Custom High-Speed Unmanned Aircraft Projects
Customized power solution for special unmanned platforms with custom airframe, flight envelope and mission requirements.
Custom & Bulk Order Service for Turbojet Power System
We provide full-set support for TH-WP160 turbojet engine procurement and integration, not limited to bare engine supply.
Optional accessory package: fuel pump, ECU, ignition system, nozzle, mounting bracket and test bench.
01
Parameter fine-tuning service: adjust thrust curve, idle speed and fuel map according to your airframe flight envelope.
02
Technical training: ground test operation, pre-flight inspection, routine maintenance and fault troubleshooting.
03
Bulk delivery arrangement: stable production capacity, flexible MOQ and customized shipping & packaging for overseas clients.
04
After-sales technical support: online guidance for engine commissioning, periodic overhaul consultation.
05
FAQ
Q: What is the maximum continuous maneuver G load of TH-WP160?
A: It supports 6g continuous maneuver overload, with peak impact overload up to 25g, suitable for catapult launch and aggressive target drone maneuvers.
Q: Can TH-WP160 run stably at 12000 m altitude?
A: Yes. The engine is calibrated to maintain usable thrust at 12000 m, designed for high-altitude cruise and target simulation missions.
Q: What is the maintenance interval for this 162kgf turbojet?
A: Standard maintenance cycle is 25 flight hours. Inspection and overhaul are required once the runtime reaches the threshold.
Q: Can you adjust the thrust curve for our custom target drone?
A: Yes. Our engineering team can re-map the fuel control system to match your airframe weight, takeoff mode and mission profile.
Q: What accessories are not included in the standard bare engine?
A: Standard bare engine excludes ECU, fuel delivery system, ignition unit and mounting fixtures. We can supply full accessory kits on request.
Q: What fuel type does TH-WP160 use?
A: It works with aviation kerosene (Jet A-1 / RP-3).
Q: Is this engine compatible with air-drop launch and catapult launch?
A: Yes. Its high impact overload structure is specially reinforced for launch shock scenarios.
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