The entire fuselage is made of aviation carbon fiber composite material,with high structural strength and lightweight,suitable forvarious application scenarios such as harsh environments and heavy mission loads.
The tailless delta wing layout makes the fuselage structure simpler,easier to deploy quickly,and easier to maintain.The modular design makes its transition more convenient while also considering versatility.
Products Description
|
X40 |
|
|
overall length |
2433 mm |
|
height |
391 mm |
|
wingspan |
2140mm |
|
Body material |
Aviation carbon fiber composite Materials |
|
engine |
Gasoline engine |
|
Load capacity |
40kg |
|
Maximum safe takeoff weight |
140 kg |
|
Safe levelflight speed |
40-65 m/s |
|
Cruise speed |
50 m/s |
|
Diving speed |
58 m/s |
|
Full load fuel consumption |
16L/h |
|
Maximum range |
675 km |
|
Practical ceiling |
4000 m |
|
Usage temperature |
-20°C-45°CC |
|
Wind resistance level |
Level 5 takeoff and landing/Level 6 flight |
|
Body protection level |
IPX4 |
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