Turbojet engine 135KG thrust HX-1350N
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Turbojet engine 135KG thrust HX-1350N
Technical indicators
ITEM |
Technical indicators |
ITEM |
Technical indicators |
Maximum thrust |
135daN |
Maximum continuous thrust |
120daN |
Maximum speed |
46000r/min |
Fuel consumption rate |
4.6L/min |
Maximum length |
750mm |
|
|
Maximum outside diameter |
265mm |
Nozzle diameter |
130mm |
N.W |
24kg |
G.W |
27kg |
Exhaust temperature |
≤800℃ |
Idling |
25000r/min |
Ground start time |
≤120s |
Push weight ratio |
5 |
service life |
≤24h |
Storage life |
5yearsq |
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