The mission-proven mid-size jet: 60 kg thrust, a 12,000 m ceiling, 20 G catapult-launch survival and 300 m/s maximum airspeed — engine, ECU(V5) and GSU integrate into one drop-in propulsion package.
Highlights
Rated 20 G longitudinal on launch — designed around real Expeditionary launchers.
12,000 m operating ceiling with full ECU control authority.
Aviation kerosene or diesel with 3–5% lubricant — logistics-friendly fuel logic.
Applications
Jet target & decoy systems · High-speed reconnaissance drones · Catapult-launched strike trainers
Product Images
Full Specifications
| Item | Value | Evidence |
|---|---|---|
| Type | Turbojet | Manufacturer spec |
| Thrust | 60 kg | Manufacturer spec |
| Dimensions | φ177 × 452 mm | Manufacturer spec |
| Weight | 6,800 g; ECU(V5) 910 g | Manufacturer spec |
| Operating temperature | −40 to +50 °C | Manufacturer spec |
| Ceiling | 12,000 m | Manufacturer spec |
| Catapult load | 20 G longitudinal | Manufacturer spec |
| Max airspeed | 300 m/s | Manufacturer spec |
| Supply voltage | 18–32 V | Manufacturer spec |
| Speed range | 25,000–72,000 rpm | Manufacturer spec |
| Rated EGT | 750 °C | Manufacturer spec |
| Max-throttle consumption | 1,735 g/min | Manufacturer spec |
| Fuel / lubrication | Aviation kerosene or diesel + 3–5% oil | Manufacturer spec |
| Service interval | 25 h | Manufacturer spec |
FAQ
Why the 20 G rating matters?
Catapult launches spike longitudinal load — the SW600Pro is rated for 20 G so the launcher choice doesn’t limit the airframe.
Diesel or kerosene?
Both run with 3–5% lubricant mix — pick per theater logistics.
Control integration?
ECU(V5) exposes RS232/RS422 and PWM; throttle protocol and GSU data logging are documented in the integration package.