The LT300 turbojet engine is a high‑performance miniature power unit designed for civilian aerial equipment. With streamlined outer dimension of 133 mm diameter and 359 mm overall length, this compact power plant balances strong thrust‑weight ratio and portable body size. It adopts mature centrifugal rotor technology and independent automatic ignition system, capable of steady long‑time operation under complex outdoor working surroundings. This engine is widely applied for recreational aircraft, large‑scale civilian drone, aerial‑photography carriers and experimental aviation projects.
| Parameter | Detailed Data |
|---|---|
| Maximum Thrust | 300 N, thrust‑to‑weight ratio 30 N/kg |
| Net Weight | 2850 g |
| Outer Diameter | 133 mm |
| Overall Length | 359 mm |
| Maximum Rated Rotation Speed | 113000 rpm |
| Idle Operating Speed | 35000 rpm |
| Max Fuel Consumption | 768 g per minute |
| Maximum Exhaust Temperature | 750℃ |
| Ignition Mode | Full‑automatic fuel ignition |
| Available Fuel Type | Aviation kerosene, diesel fuel, multiple kinds of combustible gas |
Each LT300 turbojet engine will go through strict running‑inspection before packaging. The complete set is fixed inside shock‑resistant foam case to avoid collision damage during long‑distance transit. Outer carton with waterproof wrapping protects goods against dampness. Standard international shipping solutions are available, and every package contains operation manual, spare sealing parts and basic installation accessories.
Q1: What daily‑used fuel can I run on this LT300 turbojet engine?
A: This power unit works well with aviation kerosene, regular diesel and different common combustible gas. You can pick proper fuel according to your local supply condition for your civilian aircraft projects.
Q2: Do I need complicated manual steps to start this turbojet engine?
A: It supports full‑automatic fuel ignition. After you finish the fuel pipeline connection and routine inspection, the engine can finish ignition and idle‑speed operation without complex manual ignition work.
