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HT-100 Swiss Unmanned Aerial Vehicle (UAV)

HT-100

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
HT-100 Swiss Unmanned Aerial Vehicle (UAV)
Designation
HT-100
Alternate Designation
HT-100
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Edge Group
Date of Introduction
2025
Description

The HT-100 Swiss Unmanned Aerial Vehicle (UAV) is equipped with a 15 kW turbine engine that has been meticulously developed and manufactured in Switzerland. This engine is specifically tailored for aviation applications, exhibiting a fuel consumption rate of only 9 liters per hour. It is compatible with multiple fuel types, including Jet A1, JP-5, and JP-8. This configuration promotes low vibration levels, high operational reliability, and reduced maintenance requirements, facilitated by a circumferential lubrication system and a time between overhauls (TBO) of 1,000 flight hours. The aircraft employs a dual-rotor Flettner system, which negates the need for a tail rotor and reduces energy consumption by an estimated 30% while carrying heavy payloads. The absence of mechanical components in the tail boom, combined with a modular structure, significantly enhances the aircraft's transportability and storage capabilities, including deployment on naval platforms. Regarding operational capabilities, the HT-100 can accommodate a payload of up to 60 kg, with flight durations ranging from 1 to 6 hours, contingent upon the load. The aircraft attains a maximum airspeed of 120 km/h and is capable of operating at altitudes of up to 4,000 meters, while withstanding wind speeds of up to 45 km/h. Both take-off and landing procedures are fully autonomous. The communication system employs an encrypted MESH IP data link, with options for SATCOM and LTE integration to meet specific mission requirements. Safety is a paramount consideration in the architecture of the HT-100. The aircraft is equipped with a pre-programmed autorotation function supported by a backup electric motor, redundancy in flight control through four actuators, an ADS-B Mode S transponder, a FLARM system, and a full-frame parachute. Additionally, it features a detect-and-avoid capability, terrain-following technology, front and bottom FPV cameras, as well as an automated return-to-home (RTH) function in the event of a GNSS failure. In support of operational activities, Anavia provides fixed-price, all-inclusive maintenance plans, ensuring that spare parts are supplied in advance to optimize availability. All technical documentation is compliant with manned aircraft certification standards. Furthermore, customized training programs are available for flight operators and maintenance personnel, enhancing their operational proficiency and expertise.

Air & Air Defense Specifications
Engine 15 kw shaft turbine
Max Speed 120.0 km/h
Endurance 6.00 hrs
Rotor Diameter 3.75 m
System
Alternate Designation HT-100
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Edge Group
Max. Flight Mission/ Payload Weight 1 hrs/51 kg; 2 hrs/43 kg; 4 hrs/28 kg; 6 hrs/14 kg
Payload and Fuel 60 kg (132 lbs)
Data link Type Fully encrypted MESH IP (SATCOM and LTE on demand)
Dimensions
Length 2.82 m
Height 1.00 m
Width 0.72 m
Rotor Diameter 3.75 m
Empty Weight 60kg (132 lbs)
Maximum Takeoff Weight 120 kg
Automotive
Engine Name INA
Engine Type 15 kw shaft turbine
Engine Power INA
Fuel Types Jet A1 – other fuel types on demand (JP-8, JP-5)
Fuel Consumption 9 liters per hour
Tank Capacity 60 liters (15.8 gallons)
Maximum Speed 120 km/h (65 kn)
Data Link Range Dependant on terrain topography and national regulations – radio and antenna configuration up to 200 km
Max Wind Speed 45 km/h (25 kn)
Service Ceiling INA
Endurance 6 hours
Details
Country of Origin Switzerland
Category UAVs
Air > UAVs
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.82 m
Width
0.72 m
Height
1 m
Weight
120 kg
Operators (1)
Switzerland
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