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Chin Feng I (Jing Feng I) Taiwanese Unmanned Aerial Vehicle (UAV)

Chin Feng I

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Chin Feng I (Jing Feng I) Taiwanese Unmanned Aerial Vehicle (UAV)
Designation
Chin Feng I
Alternate Designation
Chin Feng I; Jing Feng I
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
developed by Taiwan's National Chung-Shan Institute of Science and Technology (NCSIST)
Date of Introduction
2023
Description

The Chin Feng I (Jing Feng I) is a Taiwanese Unmanned Aerial Vehicle (UAV) classified as a tactical loitering munition, or suicide drone, developed by the National Chung-Shan Institute of Science and Technology (NCSIST). The Chin Feng I is a critical element of Taiwan's asymmetric "Hellscape" strategy, which seeks to saturate littoral zones with low-cost, precision munitions to disrupt amphibious landing operations. This "one shot, one kill" tactical system is analogous to the U.S. Switchblade 300 or 600 series and is intended for short-range coastal defense. It enables small units or unmanned surface vessels (USVs) to engage high-value targets such as landing craft, radar systems, or command elements without direct exposure to enemy fire. The deployment of the Chin Feng I signifies an evolution of Taiwan's "Porcupine Strategy." By shifting from reliance on expensive, low-quantity platforms, such as F-16s or frigates, to the integration of low-cost, high-volume disposable drones, Taiwan seeks to impose a disproportionately high logistical and operational cost on invading forces. Launching these drones from unmanned boats (USVs) further reduces personnel risk and preserves combat power for sustained resistance.

Air & Air Defense Specifications
Engine Electric
Range 8.0 km
Endurance 15.00 hrs
System
Alternate Designation Chin Feng I; Jing Feng I
Type Unmanned Aerial Vehicle (UAV)
Manufacturer developed by Taiwan's National Chung-Shan Institute of Science and Technology (NCSIST).
Payload Capacity INA
Airframe The drone features a folding-wing design stored inside a compact launch tube. Upon ejection via high-pressure gas, the wings snap open, and an electric motor engages to propel the drone.
Platform M96 Fast Boats, Kuai Chi USVs, Land-based trucks/tripods
AI-Assisted Terminal Guidance The sensor suite includes Electro-Optical/Infrared (EO/IR) cameras for day/night operations. The onboard AI "boxes" potential targets on the operator's tablet, allowing the human operator to select a specific target (human-in-the-loop) before the drone enters its terminal dive.
Warhead High-Explosive (HE)
Proximity Detonation A key feature demonstrated in testing is an airburst mode. If a direct hit is unlikely or if the target is a soft cluster (e.g., exposed troops on a beach or fast attack craft), the drone can detonate in close proximity to maximize fragmentation damage.
Launch Method Pneumatic tube launch (high-pressure gas)
Dimensions
Length INA
Height INA
Wingspan INA
Maximum Takeoff Weight INA
Automotive
Engine Name INA
Engine Type Electric Propeller
Engine Power INA
Maximum Speed INA
Cruise Speed INA
Maximum Range 8 km
Service Ceiling INA
Endurance 15 min
Details
Country of Origin Taiwan
Category UAVs
Air > UAVs
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Operators (2)
United States
Taiwan
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