
Technical Specification Sheet
HT-400N-A1 / 2026
Active Propulsion System
Typhoon 400N
High-precision turbojet engine engineered for professional UAV systems and tactical aerospace applications. Precision balanced to 0.01g.

Max RPM
100,000
Thrust
400N
Technical Datasheet
Reference ID: HT-JET-400-A1
Max power outputrocket_launch
400N
Weightmonitor_weight
3kg
Operational Rangespeed
100,000MAX RPM
Engineering Specifications
Fuel flow @max RPM1.35 L/min
Dimensions149mm (diameter) x 348mm
Max EGT temperature800°C
Run time @max RPM10 hours
FuelJet A-1 fuel with 5% mix of Mobile Jet Oil II
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Advanced Metallurgy & Precision Machining
The HT-400N utilizes a proprietary nickel-chromium superalloy for the turbine wheel, enabling continuous operation at extreme temperatures without creep or thermal fatigue.
- check_circleDynamic BalancingEvery rotor is balanced to G0.4 standard for vibration-free operation.
- check_circleIntegrated ECUProprietary logic for fuel management and real-time telemetry output.