The LT200 turbojet engine is a lightweight miniature jet power plant specially engineered for civilian aerial equipment. With 113‑millimeter outer diameter and 310‑millimeter total length, the streamlined body saves plenty of installation space inside aircraft frames. This jet motor adopts mature centrifugal compression technology and independent automatic ignition module, which can sustain long‑hour stable running in complicated outdoor climate. It is widely adopted for entertainment aircraft, medium‑size civilian UAVs, aerial‑shooting carriers and small‑scale aviation experimental projects.
| Parameter | Detailed Data |
|---|---|
| Maximum Thrust | 200 N, thrust‑to‑weight ratio 20 N/kg |
| Net Weight | 1860 g |
| Outer Diameter | 113 mm |
| Overall Length | 310 mm |
| Maximum Rated Rotation Speed | 115000 rpm |
| Idle Operating Speed | 36000 rpm |
| Max Fuel Consumption | 562 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 |
Every LT200 turbojet engine will pass strict runtime performance inspection before formal packaging. The whole engine set is fixed inside impact‑resistant foam casing to prevent structural damage caused by collision during long‑distance transportation. The outer waterproof carton can guard the machine against damp and dust. International‑friendly delivery solutions are supported. Each delivery package contains detailed operation handbook, backup sealing fittings and basic installation components.
Q1: Which fuels are suitable to drive the LT200 micro turbojet engine?
A: This power device is compatible with aviation kerosene, regular diesel and multiple common combustible gas. You are allowed to select proper fuel resources according to your local supply condition for civilian flying activities.
Q2: Is professional complicated operation needed when starting this turbojet motor?
A: It is fitted with the full‑automatic fuel ignition function. After you complete fuel‑pipe connection and routine safety inspection, the engine will finish ignition and idle‑speed operation without troublesome manual ignition steps.
