LF40 that is a single-shaft turbojet engine with a single-stage radial compressor is used as a kind of power plant for up to 395N thrust. It features advanced technology, high cost performance and reliability, and
can be used onunmanned aerial vehicles and missiles.It's easy to use and maintain.
Technical indicators:
|
Maximum thrust |
395±5N |
|
Operating speed |
30,000rpm~ 100,000rpm |
|
Exhaust temperature |
< 900℃ |
|
Operating altitude |
300~9,000m |
|
Operating airspeed |
0~0.8Ma |
|
Specific fuel consumption |
1210ml/min |
|
Weight |
3.3kg |
|
Jet fuel |
RP-3 |
|
Outside dimensions |
|
|
Biggest diameter |
147mm |
|
Length |
304mm |
|
Permitted fight loads |
|
|
Axial |
±20g |
|
Normal |
±6g |
|
Starting ambient temperature |
-40℃~+50℃ |
|
Operating ambient temperature: |
-50℃~+50℃ |
|
Nominal supply voltage |
12V~13.2V |
|
Cycle of the first restoration |
50h |